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  • Fluid Mechanics and Thermodynamics  (1,228)
  • AERODYNAMICS
  • Cell & Developmental Biology
  • Fisheries
  • Inorganic Chemistry
  • Limnology
  • Seismicity
  • unknown
  • 2000-2004  (2,002)
  • 1945-1949  (1,171)
Collection
Keywords
Years
Year
  • 101
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    In:  Geophys. Res. Lett., Warszawa, Pergamon, vol. 31, no. 11, pp. 837-843, pp. L11614, (ISBN: 0534351875, 2nd edition)
    Publication Date: 2004
    Keywords: Stress ; Seismicity ; Seismology ; Tectonics ; GRL ; no ; given ; name ; for ; Kalpna ; ! ; 7209 ; Seismology: ; Earthquake ; dynamics ; and ; mechanics ; 7230 ; Seismicity ; and ; seismotectonics ; 8123 ; Tectonophysics: ; Dynamics, ; seismotectonics ; 8164 ; Stresses--crust ; and ; lithosphere ; Asia
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  • 102
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    In:  Journal of Seismology, Bonn, South Afr. Inst. Mining Metall., vol. 8, no. 2, pp. 179-192, pp. 2018, (ISBN: 0534351875, 2nd edition)
    Publication Date: 2004
    Keywords: Intensity ; historical ; Seismicity ; Earthquake ; Faeh ; Fah ; JOSE
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  • 103
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    In:  Bull. Seism. Soc. Am., Bonn, Pergamon, vol. 94, no. 5, pp. 1960-1967, pp. B05S04, (ISBN: 0534351875, 2nd edition)
    Publication Date: 2004
    Keywords: Seismology ; Seismicity ; Gutenberg-Richter magnitude frequency b-value ; Recurrence of earthquakes ; Modelling ; Statistical investigations ; BSSA ; Gomez
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  • 104
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    In:  Bull. Seism. Soc. Am., Leiden, Noordhoff, vol. 94, no. 5, pp. 1579-1594, pp. 2371
    Publication Date: 2004
    Keywords: Seismology ; Earthquake hazard ; Statistical investigations ; Seismicity ; Earthquake catalog ; Error analysis ; Magnitude ; completeness ; Site amplification ; BSSA
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  • 105
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    In:  Pure and Applied Geophysics, Taipei, Elsevier, vol. 161, no. 7, pp. 1469-1487, pp. 2091, (ISBN: 0-12-018847-3)
    Publication Date: 2004
    Keywords: Geodesy ; Seismology ; Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Volcanology ; PAG ; Fernandez ; Amico
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  • 106
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    In:  Earth Science Reviews, Luxembourg, Conseil de l'Europe, vol. 65, no. 3-4, pp. 195-222, pp. B04313, (ISBN: 0-12-018847-3)
    Publication Date: 2004
    Keywords: Seismicity ; Migration of earthquakes ; Fault zone ; ESR
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  • 107
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    In:  Geophys. J. Int., Taipei, Elsevier, vol. 159, no. 3, pp. 991-1012, pp. TC1002, (ISBN: 0-12-018847-3)
    Publication Date: 2004
    Keywords: Stress ; Fault zone ; Rock mechanics ; Seismicity ; Earthquake hazard ; Subduction zone ; intraslab ; earthquake, ; seismic ; energy ; seismic ; hazard ; GJI
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  • 108
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    In:  Science, Heidelberg, 3-4, vol. 306, no. 5699, pp. 1164-1166, pp. 1516, (ISBN: 0-12-018847-3)
    Publication Date: 2004
    Keywords: Stress ; Coulomb ; Earth tides ; Seismicity
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  • 109
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    In:  J. Geophys. Res., Charleston, South Carolina, California Division of Mines San Francisco, vol. 109, no. B11, pp. 339-349, pp. B11306, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Seismicity ; Tectonics ; Geodesy ; NAF ; Fault zone ; 7215 ; Seismology: ; Earthquake ; parameters ; 7209 ; Earthquake ; dynamics ; and ; mechanics ; 7230 ; Seismicity ; and ; seismotectonics ; JGR ; 7223 ; Seismic ; hazard ; assessment ; and ; prediction
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  • 110
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    In:  Geophys. Res. Lett., Charleston, South Carolina, California Division of Mines San Francisco, vol. 31, no. 24, pp. 427-439, pp. L24604, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Subduction zone ; Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Stress ; GRL
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  • 111
    Publication Date: 2004
    Keywords: Seismology ; paleo ; historical ; Seismicity ; Fault zone ; Earthquake ; BSSA
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  • 112
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    In:  Geophys. Res. Lett., Philadelphia, 4, vol. 31, no. 2, pp. 217-230, pp. L02612, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Induced seismicity ; Fluids ; scientific drilling ; GRL
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  • 113
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    In:  Geophysical Journal International, Basle, Wiley, vol. 156, no. 2, pp. 297-306, pp. B09404, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Stress ; Italy ; Fault plane solution, focal mechanism ; GJI ; fault-plane ; solution, ; stress ; distribution
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  • 114
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    In:  Tectonophys., Basle, Wiley, vol. 385, no. 1-4, pp. 59-84, pp. B09404, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Geodesy ; Structural geology ; Switzerland
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  • 115
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    In:  Tectonophys., Dordrecht, 89, vol. 379, no. 1-4, pp. 159-181, pp. TC5003, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Geol. aspects ; China ; Tectonics ; kinematics ; Seismicity ; Tomography ; GeodesyY ; Modelling
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  • 116
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    In:  Geophysical Journal International, Washington, D.C., AGU, vol. 156, no. 3, pp. 506-526, pp. 8011, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Tectonics ; Fault plane solution, focal mechanism ; Seismology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Seismicity ; GJI
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  • 117
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    In:  Pure and Applied Geophysics, Warszawa, AGU, vol. 161, no. 7, pp. 1489-1507, pp. 2354, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Geodesy ; Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Volcanology ; Review article ; PAG ; Fernandez ; Sa ; Martins
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  • 118
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    In:  Annals Geophysics, Luxembourg, Conseil de l'Europe, vol. 47, no. 1, pp. 307-334, pp. L12309, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Earthquake catalog ; Seismicity ; Fault plane solution, focal mechanism ; Seismology
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  • 119
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    In:  J. Geophys. Res., Taipei, AGU, vol. 109, no. B8, pp. 2021-2024, pp. B08304, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Stress ; Subduction zone ; Modelling ; Fluids ; Seismicity ; JGR
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  • 120
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    In:  Geophys. Res. Lett., Taipei, AGU, vol. 31, no. 1, pp. 2021-2024, pp. L01605, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Subduction zone ; Seismicity ; Physical properties of rocks ; Magnitude ; GRL
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  • 121
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    In:  Geophys. Res. Lett., Hannover, Elsevier, vol. 31, no. 3, pp. 1-4, pp. L03605, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Earthquake ; Aftershocks ; Seismicity ; GRL ; 7215 ; Seismology: ; Earthquake ; parameters ; 7223 ; Seismic ; hazard ; assessment ; and ; prediction ; 7230 ; Seismicity ; and ; seismotectonics
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  • 122
    Publication Date: 2004
    Keywords: Earthquake ; silent ; red ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Seismicity ; Subduction zone ; Inversion ; Geodesy ; PEPI ; FLORENZO
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  • 123
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    Princeton Univ. Press
    In:  Tusla, 361 pp., Princeton Univ. Press, vol. 31, no. 3, pp. 2-203, (ISBN: 0-691-05070-8, 264 pp.)
    Publication Date: 2004
    Keywords: Earthquake ; Seismicity ; popularization ; Earthquake risk ; history
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  • 124
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    Columbia University Press
    In:  New York, 384 pp., Columbia University Press, vol. 7, no. XVI:, pp. 227-235, (ISBN 0231-12739-1 hb, 0231127383 pb)
    Publication Date: 2004
    Description: Consequences of Asthenospheric Variability in Continental Rifting, by W. Roger Buck; Velocity Fields, Faulting and Strength on the Continents, by James Jackson; Low-Angle Normal Fault Mechanics and Crustal Strength, by Gary J. Axen; Depth-Dependent Lithospheric Stretching at Rifted Continental Margins, by Mark Davis and Nick Kusznir Limits of the Seismogenic Zone, by Larry J. Ruff; Controls on Subduction Thrust Earthquakes: Downdip Changes in Composition and State, by R.D. Hyndman; Thermo-Mechanical Models of Convergent Orogenesis: Thermal and Rheologic Dependence of Crustal Deformation, by Sean D. Willett and Daniel C. Pope; Structure of Large-Displacement, Strike-Slip Fault Zones in the Brittle Continental Crust, by F.M. Chester, J.S. Chester, D.L. Kirschner, S.E. Schulz and J.P. Evans; The Strength of the San Andres Fault: A Discussion by Christopher H. Scholz and Thomas C. Hanks; Deformation Behavior of Partially Molten Mantle Rocks, by YaQin Xu, M.E. Zimmerman and D.L. Kohlstedt; Relations Among Porosity, Permeability, and Deformation in Rocks at High Temperatures, by Brian Evans, Yves Bernable and Greg Hirth --- title suggested by Tikoff: A review of seismogenic behavior in different plate tectonic settings (and some partially molten mantle deformation experiments)
    Keywords: Rheology ; Fault zone ; SAF ; Subduction zone ; Rock mechanics ; Stress ; Strength ; Plate tectonics ; Tectonics ; Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Physical properties of rocks ; Handbook of geophysics ; Strike-slip ; Dip-slip ; thrust ; convergent ; transcurrent ; divergent ; GFZ ; M ; 04.0414, ; 000268617
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  • 125
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    In:  J. Geophys. Res., Dordrecht, American Society of Civil Engineers, vol. 109, no. B9, pp. 1144-1154, pp. B09301, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Modelling ; Volcanology ; Seismicity ; Source ; Fault plane solution, focal mechanism ; Discrete / Distinct Element Method ; JGR
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  • 126
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    In:  Geophys. Res. Lett., Philadelphia, 4, vol. 31, no. 17, pp. 217-230, pp. L17609, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Statistical investigations ; Fluids ; Induced seismicity ; Modelling ; GRL
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  • 127
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    In:  J. Geophys. Res., Basle, Wiley, vol. 109, no. B6, pp. 20169-20182, pp. B06402, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Stress ; triggering ; interaction ; Strain ; Seismicity ; JGR
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  • 128
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    In:  Bull. Seism. Soc. Am., Basle, Wiley, vol. 94, no. 5, pp. 1808-1816, pp. B09404, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismology ; Hypocentral depth ; Seismicity ; Aftershocks ; BSSA
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  • 129
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    In:  Geophys. Res. Lett., Washington, D.C., AGU, vol. 31, no. 16, pp. 233-247, pp. L16602, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Earthquake ; red ; silent ; Canada ; USA ; GRL
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  • 130
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    In:  Geophys. Res. Lett., London, AGU, vol. 31, no. 15, pp. 1-1, pp. L15613, (ISSN: 1340-4202)
    Publication Date: 2004
    Description: Michelini and Lomax [2004] (hereinafter ML2004) make some statements regarding the double-difference (DD) tomography method of Zhang and Thurber [2003] (hereinafter ZT2003) that are incorrect or misleading. In this comment, we indicate the ways in which ML2004 misrepresent characteristics of ZT2003's DD tomography algorithm and the associated code tomoDD. In the process, we clarify the ways in which tomoDD differs from the DD location code hypoDD of Waldhauser [2001] and Waldhauser and Ellsworth [2000] (hereinafter WE2000).
    Keywords: Seismology ; Location ; Velocity depth profile ; Error analysis ; 7215 ; Seismology: ; Earthquake ; parameters ; GRL ; 7230 ; Seismology: ; Seismicity ; and ; seismotectonics ; 7260 ; Theory ; and ; modeling ; 8180 ; Tectonophysics: ; Tomography
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  • 131
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    In:  Annals of Geophysics, Luxembourg, Conseil de l'Europe, vol. 47, no. 1, pp. FROTH, pp. L12309, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Earthquake catalog ; Seismicity
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  • 132
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    In:  J. Geophys. Res., Veldhoven, Am. Inst. of Physics, vol. 109, no. B6, pp. 3357-3360, pp. B06304, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Stress ; Aftershocks ; Inelastic ; Rheology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Geodesy ; Seismology ; JGR ; complete ; Coulomb ; failure ; function ; slip-dependent ; friction ; 7209 ; Seismology: ; Earthquake ; dynamics ; and ; mechanics ; 7260 ; Theory ; and ; modeling ; 7230 ; Seismicity ; and ; seismotectonics ; Carli ; FROTH
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  • 133
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    In:  Geophys. Res. Lett., Washington, D.C., AGU, vol. 31, no. 7, pp. 1669-1675, pp. L07622, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Stress ; Coulomb ; Volcanology ; Seismicity ; Fault plane solution, focal mechanism ; GRL ; FROTH ; TWALTER
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  • 134
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    In:  Eos Trans. AGU, Taipei, AGU, vol. 85, no. 18, pp. 180, pp. L10613, (ISSN: 1340-4202)
    Publication Date: 2004
    Description: Coupling is a convenient word that describes a wide variety of interactions or feedback processes, including those that we do not fully understand. Examples in Earth science include ocean‐atmosphere coupling, climate-tectonics coupling, and core-mantle coupling. The word is also very popular in discussions of plate boundary earthquake processes. As a vague expression, fault coupling is a perfectly adequate term, describing some kind of mechanical interaction between rocks of each side of a fault. For those of us who try to infer fault processes from geodetic measurements, coupling usually indicates a state of no or low current slip. If a fault is fully locked, we may say it is "coupled" or "fully coupled." If a plate boundary fault is slipping at the long-term plate convergence rate, we may say it is "decoupled." Fault segments that are slipping more slowly than the plate convergence rate are then "partially" coupled. To avoid awkward expressions such as "negatively" or "overly" coupled, an equivalent description has been used in the literature, that is, to define a "coupling ratio" with values ranging from negative to greater than unity. For describing kinematics, these expressions would not be wrong. However, with one additional step, our usage of the word coupling can lead to confusion. That step is to describe a fault that is not slipping as "strongly coupled."
    Keywords: Subduction zone ; seismic Moment ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; slip ; Seismicity ; locked
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  • 135
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    In:  J. Seism. Res., Kunming, China, 3-4, vol. 27, no. 2, pp. 119-125, pp. B05301, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; China ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Earthquake precursor: deformation or strain ; Earthquake precursor: prediction research ; JSR
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  • 136
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    Cambridge Univ. Press
    In:  Cambridge, Cambridge Univ. Press, vol. 6, no. XVI:, pp. 65-70, (ISBN 0521824893, 280 pp.)
    Publication Date: 2004
    Keywords: historical ; Seismicity ; archaeology ; Earthquake hazard
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  • 137
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    In:  J. Geophys. Res., Charleston, South Carolina, California Division of Mines San Francisco, vol. 109, no. B3, pp. 8729-8744, pp. B03308, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Coulomb ; Stress ; Earthquake hazard ; Omori ; Aftershocks ; Japan ; JGR ; 7223 ; Seismology: ; Seismic ; hazard ; assessment ; and ; prediction ; 7230 ; Seismicity ; and ; seismotectonics ; 3260 ; Mathematical ; Geophysics: ; Inverse ; theory ; 8164 ; Tectonophysics: ; Stresses--crust ; and ; lithosphere ; (both) ; FROTH
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  • 138
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    In:  J. Geophys. Res., Kyoto, AGU, vol. 109, no. B2, pp. 2327-2330, pp. B02410, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Volcanology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Modelling ; Seismicity ; Earthquake ; Japan ; JGR
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  • 139
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    In:  Tectonophysics, Philadelphia, 4, vol. 390, no. 1-4, pp. 57-73, pp. 2061, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Site amplification ; NOISE ; Spectrum ; Nakamura ; Seismicity
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  • 140
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    In:  Physics of the Earth and Planetary Interiors, Hannover, Polish Geothermal Association, vol. 141, no. 4, pp. 303-326, pp. 1051, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Volcanology ; Pattern recognition ; PEPI
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  • 141
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    In:  Eos Trans. AGU, Warszawa, AGU, vol. 85, no. 14, pp. 133, 136 & 141, pp. 2354, (ISSN: 1340-4202)
    Publication Date: 2004
    Description: Large tectonic earthquakes may trigger other phenomena such as volcanic eruptions and edifice collapse, and such events in coastal areas can generate tsunamis. When closely spaced in time, these events can combine their effects to cause more serious and variable consequences than anticipated from volcanic or seismic hazards forecast separately. The Kamchatka volcanic arc, because it has been affected in the recent past by such events, provides an invaluable natural laboratory for understanding these phenomena. An international team recently studied the strong events (Mw ~ 5.5) that have occurred in Kamchatka over the last 10 k.y. The work was organized within the framework of a new NATO-Russia collaborative project studying major events occurring in volcanic arcs. It follows a joint U.S-Russian investigation carried out during 2000-2002 under the umbrella of the National Geographic Society, the U.S. National Science Foundation, and the Russian Foundation for Basic Research, which combined volcanic, geochemical, and geophysical evidence of catastrophic geological events. This work is now being built on by providing the field data necessary to understand the age, magnitude, and recurrence intervals of paleo-earthquakes, and the location, geometry, and kinematics of the main active crustal faults. Improvements in the understanding of the age and size of Holocene eruptions and refinement of their ash dispersal patterns are also being made. A multidisciplinary team is involved in this work, as well as similar studies in the Aeolian volcanic arc in Italy, thus allowing the results to be combined and compared to arrive at more general perspectives.
    Keywords: Structural geology ; paleo ; Seismicity ; Project report/description ; C14
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  • 142
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    In:  Geophysical Journal International, Taipei, AGU, vol. 157, no. 2, pp. 717-726, pp. B06410, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Modelling ; Earthquake ; Earthquake precursor: prediction research ; Earthquake precursor: chemical (Rn, water(-level,...) ; Fluids ; trigger ; Waves ; Dynamic ; Seismicity ; GJI
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  • 143
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    In:  International Journal of Rock Mechanics and Mining Sciences, Corvallis, x + 406 pp., Oregon State University Press, vol. 41, no. 8, pp. 1317-1327, pp. L13610, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Seismicity ; Statistical investigations ; Induced seismicity ; Rock mechanics ; Mining geophysics ; IJRM
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  • 144
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    Oregon State University Press
    In:  Corvallis, 2nd edition, 390 pp., Oregon State University Press, vol. 4, no. 1, pp. 1-40, (ISBN 0-87071-024-9)
    Publication Date: 2004
    Keywords: Textbook of geophysics ; Seismicity ; protection ; risk ; reduction
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  • 145
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    In:  Proceedings of the IWAM04, Mizunami, Japan, Lawrence Livermore National Laboratory, vol. 339-350, no. S3-09, 6 pp., pp. 344, (ISBN 3-933346-037)
    Publication Date: 2004
    Keywords: Tectonics ; Aegean, ; active ; faulting ; and ; monitoring, ; current ; plate ; interactions, ; Dead-Sea ; fault, ; earthquake ; source ; mechanisms ; earthquake ; potential ; and ; risk ; eastern ; Mediterranean ; region, ; InSAR, ; Sea ; of ; Marmara, ; North ; and ; East ; Anatolian ; Fault ; Zones, ; sea-bottom, ; seismology, ; seismotectonics, ; seismic ; hazard, ; Fault zone ; NAF ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Geol. aspects ; Seismicity ; Turkey ; Earthquake hazard ; Source
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  • 146
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    In:  Earth Planets Space, Washington, D.C., AGU, vol. 56, no. 16, pp. 511-515, pp. 2211, (ISSN: 1340-4202)
    Publication Date: 2004
    Keywords: Earth tidesS ; TIDES ; Seismicity ; Statistical investigations ; Correlation ; EPS
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  • 147
    Publication Date: 2004-11-13
    Description: The multibillion-dollar trade in bushmeat is among the most immediate threats to the persistence of tropical vertebrates, but our understanding of its underlying drivers and effects on human welfare is limited by a lack of empirical data. We used 30 years of data from Ghana to link mammal declines to the bushmeat trade and to spatial and temporal changes in the availability of fish. We show that years of poor fish supply coincided with increased hunting in nature reserves and sharp declines in biomass of 41 wildlife species. Local market data provide evidence of a direct link between fish supply and subsequent bushmeat demand in villages and show bushmeat's role as a dietary staple in the region. Our results emphasize the urgent need to develop cheap protein alternatives to bushmeat and to improve fisheries management by foreign and domestic fleets to avert extinctions of tropical wildlife.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Brashares, Justin S -- Arcese, Peter -- Sam, Moses K -- Coppolillo, Peter B -- Sinclair, A R E -- Balmford, Andrew -- New York, N.Y. -- Science. 2004 Nov 12;306(5699):1180-3.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Conservation Biology Group, Department of Zoology, University of Cambridge, Cambridge CB2 3EJ, UK. brashares@nature.berkeley.edu〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15539602" target="_blank"〉PubMed〈/a〉
    Keywords: Agriculture ; Animals ; *Animals, Wild ; Biodiversity ; Biomass ; Commerce ; Conservation of Natural Resources ; Fisheries ; *Fishes ; *Food Supply ; Ghana ; Humans ; *Mammals ; *Meat ; Population Density ; Population Dynamics
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 148
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    American Association for the Advancement of Science (AAAS)
    Publication Date: 2004-08-31
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Grimm, David -- New York, N.Y. -- Science. 2004 Aug 27;305(5688):1235.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15333821" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Biodiversity ; *Ecosystem ; Fisheries ; *Fishes ; Humans ; Population Density ; *Recreation ; United States
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 149
    Publication Date: 2004-09-14
    Description: It is now widely accepted that global warming is occurring, yet its effects on the world's largest ecosystem, the marine pelagic realm, are largely unknown. We show that sea surface warming in the Northeast Atlantic is accompanied by increasing phytoplankton abundance in cooler regions and decreasing phytoplankton abundance in warmer regions. This impact propagates up the food web (bottom-up control) through copepod herbivores to zooplankton carnivores because of tight trophic coupling. Future warming is therefore likely to alter the spatial distribution of primary and secondary pelagic production, affecting ecosystem services and placing additional stress on already-depleted fish and mammal populations.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Richardson, Anthony J -- Schoeman, David S -- New York, N.Y. -- Science. 2004 Sep 10;305(5690):1609-12.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Sir Alister Hardy Foundation for Ocean Science, The Laboratory, Citadel Hill, Plymouth, PL1 2PB, UK. anr@sahfos.ac.uk〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15361622" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Atlantic Ocean ; *Climate ; Copepoda/*growth & development ; *Ecosystem ; Fisheries ; Fishes ; *Food Chain ; Greenhouse Effect ; Meta-Analysis as Topic ; Phytoplankton/*growth & development ; Population Dynamics ; Seawater ; Temperature ; Zooplankton/*growth & development
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 150
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    American Association for the Advancement of Science (AAAS)
    Publication Date: 2004-08-25
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Proffitt, Fiona -- New York, N.Y. -- Science. 2004 Aug 20;305(5687):1090.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15326320" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Birds/*physiology ; *Ecosystem ; *Eels ; Fisheries ; Food Chain ; North Sea ; Plankton ; Population Density ; *Reproduction ; Scotland ; Seawater ; Temperature
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 151
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    American Association for the Advancement of Science (AAAS)
    Publication Date: 2004-06-26
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Wright, Bruce A -- Okey, Thomas A -- New York, N.Y. -- Science. 2004 Jun 25;304(5679):1903.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15218125" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; *Conservation of Natural Resources ; *Ecosystem ; *Environment ; Fisheries ; Humans ; Information Dissemination ; Population Growth ; Public Policy
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 152
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    Unknown
    American Association for the Advancement of Science (AAAS)
    Publication Date: 2004-08-25
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Allison, Edward H -- Seeley, Janet A -- New York, N.Y. -- Science. 2004 Aug 20;305(5687):1104.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15326332" target="_blank"〉PubMed〈/a〉
    Keywords: Asia/epidemiology ; Female ; Fisheries ; HIV Infections/*epidemiology/transmission ; Humans ; Male ; Occupations ; Prevalence ; Sexual Partners ; *Transients and Migrants
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 153
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    American Association for the Advancement of Science (AAAS)
    Publication Date: 2004-07-27
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Rembold, Christopher M -- New York, N.Y. -- Science. 2004 Jul 23;305(5683):475; author reply 475.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15273376" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Coronary Artery Disease/mortality/*prevention & control ; *Diet ; Environmental Pollutants/toxicity ; Fatty Acids, Omega-3/*administration & dosage ; Fisheries ; *Food Contamination ; Humans ; Neoplasms/chemically induced/epidemiology ; Randomized Controlled Trials as Topic ; Risk Assessment ; *Salmon ; Toxicity Tests
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 154
    Publication Date: 2004-09-14
    Description: 〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Stokstad, Erik -- New York, N.Y. -- Science. 2004 Sep 10;305(5690):1548-9.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/15361593" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Atlantic Ocean ; *Climate ; *Ecosystem ; Fisheries ; *Food Chain ; Phytoplankton/*growth & development ; Population Dynamics ; Seawater ; Temperature ; Zooplankton/*growth & development
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 155
    Publication Date: 2013-08-31
    Description: During the period December 23,1997 and December August 31,2004, we accomplished the development of 2 CFD codes for DNS/LES/RANS simulation of turbine cascade flows, namely LESTool and UNCLE. LESTool is a structured code making use of 5th order upwind differencing scheme and UNCLE is a second-order-accuracy unstructured code. LESTool has both Dynamic SGS and Spalart's DES models and UNCLE makes use of URANS and DES models. The current report provides a description of methodologies used in the codes.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 156
    Publication Date: 2013-08-31
    Description: The Hubble Space Telescope (HST) was launched April 24, 1990, and was deployed April 25 into low Earth orbit (LEO). It was soon discovered that the metal poles holding the solar arrays were expanding and contracting as the telescope orbited the Earth passing between the sunlight and the Earth s shadow. The expansion and contraction, although very small, was enough to cause the telescope to shake because of thermal-induced jitters, a detrimental effect when trying to take pictures millions of miles away. Therefore, the European Space Agency (ESA, the provider of the solar arrays) built new solar arrays (SA-11) that contained bi-stem thermal shields which insulated the solar array metal poles. These thermal shields were made of 2 mil thick aluminized-Teflon fluorinated ethylene propylene (FEP) rings fused together into a circular bellows shape. The new solar arrays were put on the HST during an extravehicular activity (EVA), also called an astronaut space walk, during the first servicing mission (SM1) in December 1993. An on-orbit photograph of the HST with the SA-11, and a close up of the bellows-like structure of the thermal shields is provided in Figure 1.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Interm Summary Reports
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  • 157
    Publication Date: 2018-06-12
    Description: A computational heat transfer design methodology was developed to study the dual-engine linear aerospike plume-induced base-heating environment during one power-pack out, in ascent flight. It includes a three-dimensional, finite volume, viscous, chemically reacting, and pressure-based computational fluid dynamics formulation, a special base-bleed boundary condition, and a three-dimensional, finite volume, and spectral-line-based weighted-sum-of-gray-gases absorption computational radiation heat transfer formulation. A separate radiation model was used for diagnostic purposes. The computational methodology was systematically benchmarked. In this study, near-base radiative heat fluxes were computed, and they compared well with those measured during static linear aerospike engine tests. The base-heating environment of 18 trajectory points selected from three power-pack out scenarios was computed. The computed asymmetric base-heating physics were analyzed. The power-pack out condition has the most impact on convective base heating when it happens early in flight. The source of its impact comes from the asymmetric and reduced base bleed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Journal of Propulsion and Power (ISSN 0748-4658); Volume 20; No. 3; 385-393
    Format: text
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  • 158
    Publication Date: 2018-06-11
    Description: This paper details a novel three-dimensional (3D) hydro-focusing micro cell sorter for micro flow cytometry applications. The unit was microfabricated by means of SU-8 3D lithography. The 3D microstructure for coaxial sheathing was designed, microfabricated, and tested. Three-dimensional hydro-focusing capability was demonstrated with an experiment to sort labeled tanned sheep erythrocytes (red blood cells). This polymer hydro-focusing microstructure is easily microfabricated and integrated with other polymer microfluidic structures.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 159
    Publication Date: 2018-06-05
    Description: The Sensors and Electronics Technology Branch of the NASA Glenn Research Center is developing thin-film-based sensors for surface measurement in propulsion system research. Thin-film sensors do not require special machining of the components on which they are mounted, and they are considerably thinner than wire- or foil-based sensors. One type of sensor being advanced is the thin-film thermocouple, specifically for applications in high-temperature combustion environments. Ceramics are being demonstrated as having the potential to meet the demands of thin-film thermocouples in advanced aerospace environments. The maximum-use temperature of noble metal thin-film thermocouples, 1500 C (2700 F), may not be adequate for components used in the increasingly harsh conditions of advanced aircraft and next-generation launch vehicles. Ceramic-based thermocouples are known for their high stability and robustness at temperatures exceeding 1500 C, but are typically in the form of bulky rods or probes. As part of ASTP, Glenn's Sensors and Electronics Technology Branch is leading an in-house effort to apply ceramics as thin-film thermocouples for extremely high-temperature applications as part of ASTP. Since the purity of the ceramics is crucial for the stability of the thermocouples, Glenn's Ceramics Branch and Case Western Reserve University are developing high-purity ceramic sputtering targets for fabricating high-temperature sensors. Glenn's Microsystems Fabrication Laboratory, supported by the Akima Corporation, is using these targets to fabricate thermocouple samples for testing. The first of the materials used were chromium silicide (CrSi) and tantalum carbide (TaC). These refractory materials are expected to survive temperatures in excess of 1500 C. Preliminary results indicate that the thermoelectric voltage output of a thin-film CrSi versus TaC thermocouple is 15 times that of the standard type R (platinum-rhodium versus platinum) thermocouple, producing 20 mV with a 200 C temperature gradient. The photograph on the left shows the CrSi-TaC thermocouple in a test fixture at Glenn, and the resulting output signal is shown on the right. The temperature differential across the sample, from the center of the sample inside the oven to the sample mount outside the oven, is measured using a type R thermocouple on the sample.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 160
    Publication Date: 2018-06-05
    Description: The unsteady, incompressible Navier-Stokes equations are used for the direct numerical simulation (DNS) of spatially evolving disturbances in a three-dimensional (3-D) attachment-line boundary layer. Two-dimensional (2-D) disturbances are introduced either by forcing at the in ow or by harmonic-source generators at the wall; 3-D disturbances are introduced by harmonic-source generators at the wall. The DNS results are in good agreement with both 2-D non-parallel theory (for small-amplitude disturbances) and weakly nonlinear theory (for finite-amplitude disturbances), which validates the two theories. The 2-D DNS results indicate that nonlinear disturbance growth occurs near branch II of the neutral stability curve; however, steady suction can be used to stabilize this disturbance growth. For 3-D instabilities that are generated o the attachment line, spreading both toward and away from the attachment line causes energy transfer to the attachment-line and downstream instabilities; suction stabilizes these instabilities. Furthermore, 3-D instabilities are more stable than 2-D or quasi-2-D instabilities.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 161
    Publication Date: 2018-06-05
    Description: A fast multigrid solver for the steady incompressible Euler equations is presented. Unlike time-marching schemes, this approach uses relaxation of the steady equations. Application of this method results in a discretization that correctly distinguishes between the advection and elliptic parts of the operator, allowing efficient smoothers to be constructed. Solvers for both unstructured triangular grids and structured quadrilateral grids have been written. Computations for channel flow and flow over a nonlifting airfoil have computed. Using Gauss-Seidel relaxation ordered in the flow direction, textbook multigrid convergence rates of nearly one order-of-magnitude residual reduction per multigrid cycle are achieved, independent of the grid spacing. This approach also may be applied to the compressible Euler equations and the incompressible Navier-Stokes equations.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 162
    Publication Date: 2018-06-12
    Description: The structural analysis results for a graphite/epoxy quasi-isotropic circular plate subjected to a forced rotation at the boundary and pressure is presented. The analysis is to support a specialized material characterization test for composite cryogenic tanks. Finite element models were used to ensure panel integrity and determine the pressure necessary to achieve a predetermined equal biaxial strain value. The displacement results due to the forced rotation at the boundary led to a detailed study of the bending stiffness matrix [D]. The variation of the bending stiffness terms as a function of angular position is presented graphically, as well as, an illustrative technique of considering the laminate as an I-beam.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 163
    Publication Date: 2018-06-06
    Description: Various artificial compressibility methods for calculating the three-dimensional incompressible Navier-Stokes equations are compared. Each method is described and numerical solutions to test problems are conducted. A comparison based on convergence behavior, accuracy, and robustness is given.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 164
    Publication Date: 2018-06-06
    Description: This study provides systematic method for reducing power consumption in reduced gravity systems by adopting minimum velocity required to provide adequate CHF and preclude detrimental effects of reduced gravity . This study proves it is possible to use existing 1 ge flow boiling and CHF correlations and models to design reduced gravity systems provided minimum velocity criteria are met
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Presentations, Volume 1; 710-737; NASA/CP-2004-213205/VOL1
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  • 165
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    In:  CASI
    Publication Date: 2018-06-06
    Description: Recent workshops to define strategic research on critical issues in microgravity fluids and transport phenomena in support of mission orientated needs of NASA and many technical conferences over the years in support of fundamental research targeting NASA's long range missions goal have identified several phase change processes needed to design advanced space and planetary based systems for long duration operations Recommendation noted that phase change processes are profoundly affected by gravitational environment.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Presentations, Volume 1; 255-268; NASA/CP-2004-213205/VOL1
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  • 166
    Publication Date: 2018-06-06
    Description: We present experimental data on flow pattern transitions, pressure drop and flow characteristics for cocurrent gas-liquid flow through packed columns in microgravity. The flow pattern transition data indicates that the pulse flow regime exists over a wider range of gas and liquid flow rates under microgravity conditions compared to 1-g and the widely used Talmor map in 1-g is not applicable for predicting the transition boundaries. A new transition criterion between bubble and pulse flow in microgravity is proposed and tested using the data. Since there is no static head in microgravity, the pressure drop measured is the true frictional pressure drop. The pressure drop data, which has much smaller scatter than most reported 1-g data clearly shows that capillary effects can enhance the pressure drop (especially in the bubble flow regime) as much as 200% compared to that predicted by the single phase Ergun equation. The pressure drop data are correlated in terms of a two-phase friction factor and its dependence on the gas and liquid Reynolds numbers and the Suratman number. The influence of gravity on the pulse amplitude and frequency is also discussed and compared to that under normal gravity conditions. Experimental work is planned to determine the gas-liquid and liquid-solid mass transfer coefficients. Because of enhanced interfacial effects, we expect the gas-liquid transfer coefficients kLa and kGa (where a is the gas-liquid interfacial area) to be higher in microgravity than in normal gravity at the same flow conditions. This will be verified by gas absorption experiments, with and without reaction in the liquid phase, using oxygen, carbon dioxide, water and dilute aqueous amine solutions. The liquid-solid mass transfer coefficient will also be determined in the bubble as well as the pulse flow regimes using solid benzoic acid particles in the packing and measuring their rate of dissolution. The mass transfer coefficients in microgravity will be compared to those in normal gravity cocurrent flow to determine the mass transfer enhancement and propose new mass transfer correlations for two-phase gas-liquid flows through packed beds in microgravity.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Presentations, Volume 1; 695-709; NASA/CP-2004-213205/VOL1
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  • 167
    Publication Date: 2018-06-06
    Description: One particular characteristic observed in unsteady shear layers is the phase shift relative to the main flow. In attached boundary layers this will have an effect both on the instantaneous skin friction and heat transfer. In separation bubbles the contribution to the drag is dominated by the pressure distribution. However, the most significant effect appears to be the phase shift on the transition process. Unsteady transition behaviour may determine the bursting of the bubble resulting in an un-recoverable full separation. An early analysis of the phase shift was performed by Stokes for the incompressible boundary layer of an oscillating wall and an oscillating main flow. An amplitude overshoot within the shear layer as well as a phase shift were observed that can be attributed to the relatively slow diffusion of viscous stresses compared to the fast change of pressure. Experiments in a low speed facility with the boundary layer of a flat plate were evaluated in respect to phase shift. A pressure distribution similar to that on the suction surface of a turbomachinery aerofoil was superimposed generating a typical transitional separation bubble. A periodically unsteady main flow in the suction type wind tunnel was introduced via a rotating flap downstream of the test section. The experiments covered a range of the three similarity parameters of momentum-loss-thickness Reynolds-number of 92 to 226 and Strouhal-number (reduced frequency) of 0.0001 to 0.0004 at the separation point, and an amplitude range up to 19 %. The free stream turbulence level was less than 1% .Upstream of the separation point the phase shift in the laminar boundary layer does not appear to be affected significantly bay either of the three parameters. The trend perpendicular to the wall is similar to the Stokes analysis. The problem scales well with the wave velocity introduced by Stokes, however, the lag of the main flow near the wall is less than indicated analytically. The separation point comes closest to the Stokes analysis but the phase is still 20 degrees lower at the wall.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Minnowbrook IV: 2003 Workshop on Transition and Unsteady Aspects of Turbomachinery Flows; 54-55; NASA/TM-2004-212913
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  • 168
    Publication Date: 2018-06-06
    Description: Among the numerous causes for unsteadiness in turbo machinery flows are turbulence and flow environment, wakes from stationary and rotating vanes, boundary layer separation, boundary layer/shear layer instabilities, presence of shock waves and deliberate unsteadiness for flow control purposes. These unsteady phenomena may lead to flow-structure interactions such as flutter and forced vibration as well as system instabilities such as stall and surge. A major issue of unsteadiness relates to the fact that a fundamental understanding of unsteady flow physics is lacking and requires continued attention. Accurate simulations and sufficient high fidelity experimental data are not available. The Glenn Research Center plan for Engine Component Flow Physics Modeling is part of the NASA 21st Century Aircraft Program. The main components of the plan include Low Pressure Turbine National Combustor Code. The goals, technical output and benefits/impacts of each element are described in the presentation. The specific areas selected for discussion in this presentation are blade wake interactions, flow control, and combustor exit turbulence and modeling.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Minnowbrook IV: 2003 Workshop on Transition and Unsteady Aspects of Turbomachinery Flows; 3-27; NASA/TM-2004-212913
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  • 169
    Publication Date: 2018-06-06
    Description: The Effects of elevated free-stream turbulence (FST) on the natural and periodically excited separation bubbles were studied experimentally, due to the relevance of this flow to low-pressure turbine blades at low Reynolds numbers. A bubble was formed at the leading edge of a flat plate and the FST level was altered by placing a grid across the flow at different locations upstream of the plate. The mixing across the separated shear-layer, forming the free boundary of the bubble, increased due to the elevated FST and due to nominally two-dimensional periodic excitation, both flattening and shortening the bubble. Periodic excitation at frequencies that were at least an order of magnitude lower than those associated with the initial shear-layer instability, were very effective at low FST, because the amplitudes of the excitation frequency and its harmonic were amplified over the bubble. High frequency excitation (F+ 3, based on the length of the baseline low FST bubble) had a major effect close to the separation location, while farther downstream the excited fluctuations rapidly decayed in the reattachment region. Low frequency excitation, that generated waves comparable to the length of the unperturbed bubble (F+ 1) were less effective and their magnitude decayed at a slower rate downstream of reattachment. An increase in the level of the FST reduced the net effect of the periodic excitation on the mixing enhancement and subsequent reattachment process, probably due to a destructive interference between the nominally 2D excitation and the random (in space and time) FST, reducing the spanwise coherence and therefore the effectiveness of the current control strategy. However, even at the reduced effectiveness of 2D periodic excitation at elevated FST, it accelerated the reattachment process and the recovery rate of the reattached boundary layer, enhancing the boundary layer resistance to repeat separation and reducing its momentum loss further downstream.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Minnowbrook IV: 2003 Workshop on Transition and Unsteady Aspects of Turbomachinery Flows; 392-406; NASA/TM-2004-212913/SUPPL
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  • 170
    Publication Date: 2018-06-05
    Description: In this brief, we investigate the turbulent condensation of a population of droplets by means of a direct numerical simulation. To that end, a coupled Navier-Stokes/Lagrangian solver is used where each particle is tracked and its growth by water vapor condensation is monitored exactly. The main goals of the study are to find out whether turbulence broadens the droplet size distribution, as observed in in situ measurements. The second issue is to understand if and for how long a correlation between the droplet radius and the local supersaturation exists for the purpose of modeling sub-grid scale microphysics in cloud-resolving codes. This brief is organized as follows. In Section 2 the governing equations are presented, including the droplet condensation model. The implementation of the forcing procedure is described in Section 3. The simulation results are presented in Section 4 together with a sketch of a simple stochastic model for turbulent condensation. Conclusions and the main outcomes of the study are given in Section 5.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Annual Research Briefs, 2004: Center for Turbulence Research; 305-316
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  • 171
    Publication Date: 2018-06-02
    Description: Three-dimensional computational techniques, in particular the uncoupled CFD-DSMC of the present study, are available to be applied to problems such as jet interactions with variable density regions ranging from a continuum jet to a rarefied free stream. When the value of the jet to free stream momentum flux ratio approximately greater than 2000 for a sharp leading edge flat plate forward separation vortices induced by the jet interaction are present near the surface. Also as the free stream number density n (infinity) decreases, the extent and magnitude of normalized pressure increases and moves upstream of the nozzle exit. Thus for the flat plate model the effect of decreasing n (infinity) is to change the sign of the moment caused by the jet interaction on the flat plate surface.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 172
    Publication Date: 2018-06-02
    Description: InSPACE is a microgravity fluid physics experiment that was operated on the International Space Station (ISS) in the Microgravity Science Glovebox from late March 2003 through early July 2003. (InSPACE is an acronym for Investigating the Structure of Paramagnetic Aggregates From Colloidal Emulsions.) The purpose of the experiment is to obtain fundamental data of the complex properties of an exciting class of smart materials termed magnetorheological (MR) fluids. MR fluids are suspensions, or colloids, comprised of small (micrometer-sized) superparamagnetic particles in a nonmagnetic medium. Colloids are suspensions of very small particles suspended in a liquid. (Examples of other colloids are blood, milk, and paint.) These controllable fluids can quickly transition into a nearly solid state when exposed to a magnetic field and return to their original liquid state when the magnetic field is removed. Controlling the strength of the magnetic field can control the relative stiffness of these fluids. MR fluids can be used to improve or develop new seat suspensions, robotics, clutches, airplane landing gear, and vibration damping systems. The principal investigator for InSPACE is Professor Alice P. Gast of the Massachusetts Institute of Technology (MIT). The InSPACE hardware was developed at the NASA Glenn Research Center. The InSPACE samples were delivered to the ISS in November 2002, on the Space Shuttle Endeavour, on Space Station Utilization Flight UF-2/STS113. Operations began on March 31, 2003, with the processing of three different particle size samples at multiple test parameters. This investigation focused on determining the structural organization of MR colloidal aggregates when exposed to a pulsing magnetic field. On Earth, the aggregates take the shape of footballs with spiky tips. This characteristic shape may be influenced by the pull of gravity, which causes most particles initially suspended in the fluid to sediment, (i.e., settle and collect at the bottom of the cell). In the absence of sedimentation effects on the ISS, the behavior and shape of these MR aggregate structures are dominated exclusively by magnetic and surface tension forces. The microscopic detail of these structures was imaged under two orthogonal camera views. The video was downlinked to the InSPACE team at Glenn's Telescience Support Center and to MIT and also recorded onboard the ISS on videotapes that will be brought back to the ground by the space shuttles. The study examined the effect on the structure formation by varying the magnetic field strength and pulse frequency, and particle size. Fundamental data that characterized the structure formation were obtained. InSPACE completed its last planned test run on July 2, 2003. Operations occurred on 21 days over approximately a 3-month period. Forty-one test points were completed during 26 test runs. During the initial testing, the procedures followed by the crew were modified to maximize the observation of some unexpected and interesting aggregate behavior. As a result Dr. Gast has reported on the formation of aggregate shapes that are more extended and diverse than those observed on the ground. Sheets of magnetic material folded over in a labyrinth pattern and large columnar aggregates with complex interfaces with the surrounding fluid are examples of the interesting structures that have been observed on the ISS. In light of these early findings, the understanding of the fundamental properties of MR fluids on the basis of ground-based observations may need to be reconsidered.The experiments on the ISS have provided a vast amount of video data for analysis. While this analysis is ongoing, plans are being made for additional experimental runs. For this purpose, additional hardware and cells containing samples of different magnetic particles and sizes are being fabricated for a future launch to the ISS. The InSPACE hardware will remain on orbit until this testing is completed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 173
    Publication Date: 2018-06-02
    Description: Leakage and wear are two fundamental problems in all traditional turbine seals that contribute to an engine's inefficiency. The solutions to seal leakage and wear conflict in the conventional design space. Reducing the clearance between the seal and rotating shaft reduces leakage but increases wear because of increased contact incidents. Increasing the clearance to reduce the contact between parts reduces wear but increases parasitic leakage. The goal of this effort is to develop a seal that restricts leakage flow using acoustic pressure while operating in a noncontacting manner, thereby increasing life. In 1996, Dr. Timothy Lucas announced his discovery of a method to produce shock-free high-amplitude pressure waves. For the first time, the formation of large acoustic pressures was possible using dissonant resonators. A pre-prototype acoustic seal developed at the NASA Glenn Research Center exploits this fundamental acoustic discovery: a specially shaped cavity oscillated at the contained fluid's resonant frequency produces high-amplitude acoustic pressure waves of a magnitude approaching those required of today's seals. While the original researchers are continuing their development of acoustic pumps, refrigeration compressors, and electronic thermal management systems using this technology, the goal of researchers at Glenn is to apply these acoustic principles to a revolutionary sealing device. When the acoustic resonator shape is optimized for the sealing device, the flow from a high-pressure cavity to a low-pressure cavity will be restricted by a series of high-amplitude standing pressure waves of higher pressure than the pressure to be sealed. Since the sealing resonator cavity will not touch the adjacent sealing structures, seal wear will be eliminated, improving system life. Under a cooperative agreement between Glenn and the Ohio Aerospace Institute (OAI), an acoustic-based pre-prototype seal was demonstrated for the first time. A pressurized cavity was attached to one end of the resonator while the other end remained open to ambient pressure. Measurements were taken at several values of applied pressure with the assembly stationary, oscillated at an off-resonance frequency, and then oscillated on-resonance. The three cases show that the flow through the conical resonator can be reduced by oscillating the resonator at the resonance frequency of the air contained within the cavity. The results are currently being compared with results obtained from a commercial computational fluid dynamics code. The objective is to improve the design through numerical simulation before fabricating a next-generation prototype sealing device. Future work is aimed at implementing acoustic seal design improvements to further reduce the leakage flow rate through the device and at reducing the device's overall size.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 174
    Publication Date: 2018-06-06
    Description: A new technology for reducing turbulent skin friction, called the Microblowing Technique (MBT), is presented. Results from proof-of-concept experiments show that this technology could potentially reduce turbulent skin friction by more than 50% of the skin friction of a solid flat plate for subsonic and supersonic flow conditions. The primary purpose of this review paper is to provide readers with information on the turbulent skin friction reduction obtained from many experiments using the MBT. Although the MBT has a penalty for obtaining the microblowing air associated with it, some combinations of the MBT with suction boundary layer control methods are an attractive alternative for a real application. Several computational simulations to understand the flow physics of the MBT are also included. More experiments and computational fluid dynamics (CFD) computations are needed for the understanding of the unsteady flow nature of the MBT and the optimization of this new technology.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 175
    Publication Date: 2018-06-06
    Description: Solve the time-dependent inviscid flow equations for this geometry subject to the specified inflow/outflow mean conditions and the fluctuating inflow velocity distortion. (1) Compute the unsteady solution until periodicity in pressure is achieved by showing that at least two successive periods are identical. Periodicity must be achieved on both the airfoil surface and the inflow/outflow boundaries. (2) Once periodicity is achieved, compute the pressure frequency spectra on the reference airfoil on both the upper and lower surfaces at x=(-0.25c,0.00, +0.25c), on the inflow boundary at (x,y)={1.5c,-0.3c), (-1.5c,0.0),(-1.5c,0.3c)} and on the outflow boundary at (x,y)= {(1.5c,-0.3c),(1.5c,0.0), (1.5c,0.3c)}. Express the spectral results in dB using the standard definition 20 log(P(sub(r.m.s)/P(sub ref), where p(sub ref) == 20 microPa. (3) Extract the harmonic pressure distributions on the inflow and outflow boundaries (i.e., on x= -/+ 1.5c lines) at the fundamental frequency omega and apply a Fourier transform in y direction to identify the spatial (i.e., mode order) structure of the pressure perturbations. Express the result in dB for each mode order. Repeat the process for the frequencies 2omega and 3omega.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems; 18-22; NASA/CP-2004-212954
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  • 176
    Publication Date: 2018-06-06
    Description: Three benchmark problems from the current and previous CAA workshops involving tone noise generated in viscous flows are investigated using the CE/SE finite volume method. The CE/SE method is first briefly reviewed. Then, the benchmark problems, namely, flow past a single cylinder (CAA Workshop II problem), flow past twin cylinders (from the current CAA Workshop IV, Category 5, Problem 1) and flow past a deep cavity with overhang (CAA Workshop III problem) are investigated. Generally good results are obtained in comparison with the experimental data.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems; 213-228; NASA/CP-2004-212954
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  • 177
    Publication Date: 2018-06-06
    Description: The effects of gravity on the bubble formation in an annular jet were studied. The experiments were conducted in the 2.2-second drop tower at the NASA Glenn Research Center. Terrestrial gravity experiments were conducted at the Fluid Dynamics Research Laboratory at the University of Oklahoma. Stainless steel tubing with inner diameters of 1/8" (gas inner annulus) and 5/16" (liquid outer annulus) served as the injector. A rectangular test section, 6" x 6" x 14" tall, made out of half-inch thick Lexan was used. Images of the annular jet were acquired using a high-speed camera. The effects of gravity and varying liquid and gas flow rates on bubble size, wavelength, and breakup length were documented. In general, the bubble diameter was found to be larger in terrestrial gravity than in microgravity for varying Weber numbers (0.05 - 0.16 and 5 - 11) and liquid flow rates (1.5 ft/s - 3.0 ft/s). The wavelength was found to be larger in terrestrial gravity than in microgravity, but remained constant for varying Weber numbers. For low Weber numbers (0.05 - 0.16), the breakup length in microgravity was significantly higher than in terrestrial gravity. Comparison with linear stability analysis showed estimated bubble sizes within 9% of experimental bubble sizes. Bubble size compared to other terrestrial gravity experiments with same flow conditions showed distinct differences in bubble size, which displayed the importance of injector geometry on bubble formation.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Poster Session, Volume 2; 206-215; NASA/CP-2004-213205/VOL2
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  • 178
    Publication Date: 2018-06-06
    Description: The objective of the present study is to develop a two-fluid model formulation with interfacial area transport equation applicable for microgravity conditions. The new model is expected to make a leapfrog improvement by furnishing the constitutive relations for the interfacial interaction terms with the interfacial area transport equation, which can dynamically model the changes of the interfacial structures. In the first year of this three-year project supported by the U.S. NASA, Office of Biological and Physics Research, the primary focus is to design and construct a ground-based, microgravity two-phase flow simulation facility, in which two immiscible fluids with close density will be used. In predicting the two-phase flow behaviors in any two-phase flow system, the interfacial transfer terms are among the most essential factors in the modeling. These interfacial transfer terms in a two-fluid model specify the rate of phase change, momentum exchange, and energy transfer at the interface between the two phases. For the two-phase flow under the microgravity condition, the stability of the fluid particle interface and the interfacial structures are quite different from those under normal gravity condition. The flow structure may not reach an equilibrium condition and the two fluids may be loosely coupled such that the inertia terms of each fluid should be considered separately by use of the two-fluid model. Previous studies indicated that, unless phase-interaction terms are accurately modeled in the two-fluid model, the complex modeling does not necessarily warrant an accurate solution.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Poster Session, Volume 2; 146-157; NASA/CP-2004-213205/VOL2
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  • 179
    Publication Date: 2018-06-06
    Description: Flow regime and pressure drop data was obtained and analyzed. Pulse flow exists at lower liquid flow rates in 0-g compared to 1-g. 1-g flow regime maps do not apply in microgravity. Pressure drop is higher in microgravity (enhanced interfacial effects).
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Strategic Research to Enable NASA's Exploration Missions Conference and Workshop: Presentations, Volume 1; 2-15; NASA/CP-2004-213205/VOL1
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  • 180
    Publication Date: 2018-06-05
    Description: In fiscal year 2003, test cell 23 of the Research Combustion Laboratory (RCL 23) at the NASA Glenn Research Center was upgraded with the addition of gaseous hydrogen as a working propellant and the addition of a 450-psig air-supply system. Test flexibility was further enhanced by upgrades to the facility control systems. RCL 23 can now test with gaseous hydrogen flow rates up to 0.05 lbm/sec and jet fuel flow rates up to 0.62 lbm/sec. Research airflow rates up to 3 lbm/sec are possible with the 450-psig supply system over a range of inlet temperatures. Nonvitiated, heated air is supplied from a shell and tube heat exchanger. The maximum nonvitiated facility air temperature is 1100 F at 1.5 lbm/sec. Research-section exhaust temperatures are limited to 3200 F because of material and cooling capacity limits. A variety of support systems are available depending on the research hardware configuration. Test section ignition can be provided via either a hydrogen air torch system or an electronic spark system. Emissions measurements are obtained with either pneumatically or electromechanically actuated gas sample probes, and the electromechanical system allows for radial measurements at a user-specified axial location for measurement of emissions profiles. Gas analysis data can be obtained for a variety of species, including carbon monoxide (CO), carbon dioxide (CO2), nitrogen oxides (NO and NOx), oxygen (O2), unburnt hydrocarbons, and unburnt hydrogen. Facility control is accomplished with a programmable logic control system. Facility operations have been upgraded to a system based on graphical user interface control screens. A data system is available for real-time acquisition and monitoring of both measurements in engineering units and performance calculations. The upgrades have made RCL 23 a highly flexible facility for research into low emissions gas turbine combustor concepts, and the flame tube configuration inherently allows for a variety of fuel nozzle configurations to be tested in a cost-effective manner. RCL 23 is poised to be a leading facility for developing modern low-emission fuel nozzles for use with jet fuel and alternative fuels.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 181
    Publication Date: 2018-06-05
    Description: The operation of a packed bed reactor (PBR) involves gas and liquid flowing simultaneously through a fixed-bed of solid particles. Depending on the application, the particles can be various shapes and sizes but are generally designed to force the two fluid phases through a tortuous route of narrow channels connecting the interstitial space. The PBR is the most common type of reactor in industry because it provides for intimate contact and high rates of transport between the phases needed to sustain chemical or biological reactions. The packing may also serve as either a catalyst or as a support for growing biological material. Furthermore, this type of reactor is relatively compact and requires minimal power to operate. This makes it an excellent candidate for unit operations in support of long-duration human space activities.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 182
    Publication Date: 2018-06-05
    Description: Recent research efforts within the Microgravity Fluid Physics Branch of the NASA Glenn Research Center have necessitated the development of a microscope capable of high-resolution, three-dimensional imaging of intracellular structure and tissue morphology. Standard optical microscopy works well for thin samples, but it does not allow the imaging of thick samples because of severe degradation caused by out-of-focus object structure. Confocal microscopy, which is a laser-based scanning microscopy, provides improved three-dimensional imaging and true optical sectioning by excluding the out-of-focus light. However, in confocal microscopy, out-of-focus object structure is still illuminated by the incoming beam, which can lead to substantial photo-bleaching. In addition, confocal microscopy is plagued by limited penetration depth, signal loss due to the presence of a confocal pinhole, and the possibility of live-cell damage. Two-photon microscopy is a novel form of laser-based scanning microscopy that allows three-dimensional imaging without many of the problems inherent in confocal microscopy. Unlike one-photon microscopy, it utilizes the nonlinear absorption of two near-infrared photons. However, the efficiency of two-photon absorption is much lower than that of one-photon absorption because of the nonlinear (i.e., quadratic) electric field dependence, so an ultrafast pulsed laser source must typically be employed. On the other hand, this stringent energy density requirement effectively localizes fluorophore excitation to the focal volume. Consequently, two-photon microscopy provides optical sectioning and confocal performance without the need for a signal-limiting pinhole. In addition, there is a reduction in photo-damage because of the longer excitation wavelength, a reduction in background fluorescence, and a 4 increase in penetration depth over confocal methods because of the reduction in Rayleigh scattering.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 183
    Publication Date: 2018-06-05
    Description: Many valuable advances in combustion science have come from observations of microgravity flames. This research is contributing to the improved efficiency and reduced emissions of practical combustors and is benefiting terrestrial and spacecraft fire safety. Unfortunately, difficulties associated with microgravity have prevented many types of measurements in microgravity flames. In particular, temperature measurements in flames are extremely important but have been limited in microgravity. A novel method of measuring temperatures in microgravity flames is being developed in-house at the National Center for Microgravity Research and the NASA Glenn Research Center and is described here. Called thin-filament pyrometry, it involves using a camera to determine the local gas temperature from the intensity of inserted fibers glowing in a flame. It is demonstrated here to provide accurate measurements of gas temperatures in a flame simultaneously at many locations. The experiment is shown. The flame is a laminar gas jet diffusion flame fueled by methane (CH4) flowing from a 14-mm round burner at a pressure of 1 atm. A coflowing stream of air is used to prevent flame flicker. Nine glowing fibers are visible. These fibers are made of silicon carbide (SiC) and have a diameter of 15 m (for comparison, the average human hair is 75 m in diameter). Because the fibers are so thin, they do little to disturb the flame and their temperature remains close to that of the local gas. The flame and glowing filaments were imaged with a digital black-and-white video camera. This camera has an imaging area of 1000 by 1000 pixels and a wide dynamic range of 12 bits. The resolution of the camera and optics was 0.1 mm. Optical filters were placed in front of the camera to limit incoming light to 750, 850, 950, and 1050 nm. Temperatures were measured in the same flame in the absence of fibers using 50-m Btype thermocouples. These thermocouples provide very accurate temperatures, but they generally are not useful in microgravity tests because they measure temperature at only one location at a time. Thermocouple measurements at a height of 11 mm above the burner were used to calibrate the thin-filament pyrometry system at all four wavelengths. This calibration was used to perform thin-filament pyrometry at other heights above the burner. One such profile is shown in this graph; this is for a height of 21 mm. The agreement between the pyrometry measurements and thermocouple results at this height is excellent in the range of 1000 to 2000 K, with an estimated uncertainty of 50 K and an estimated upper limit of 2500 K. Neither the thermocouple nor the thin-filament pyrometry temperatures have been corrected for radiation, but the correction is expected to be nearly the same for both methods. We anticipate that thin-filament pyrometry similar to that developed here will become an important diagnostic for studies of microgravity flames owing to its accuracy and its ability to simultaneously measure finely spaced temperatures.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 184
    Publication Date: 2018-06-05
    Description: When discharged into an International Space Station (ISS) payload rack, a carbon dioxide (CO2) portable fire extinguisher (PFE) must extinguish a fire by decreasing the oxygen in the rack by 50 percent within 60 sec. The length of time needed for this oxygen reduction throughout the rack and the length of time that the CO2 concentration remains high enough to prevent the fire from reigniting is important when determining the effectiveness of the response and postfire procedures. Furthermore, in the absence of gravity, the local flow velocity can make the difference between a fire that spreads rapidly and one that self-extinguishes after ignition. A numerical simulation of the discharge of CO2 from PFE into the Combustion Integrated Rack (CIR) in microgravity was performed to obtain the local velocity and CO2 concentration. The complicated flow field around the PFE nozzle exits was modeled by sources of equivalent mass and momentum flux at a location downstream of the nozzle. The time for the concentration of CO2 to reach a level that would extinguish a fire anywhere in the rack was determined using the Fire Dynamics Simulator (FDS), a computational fluid dynamics code developed by the National Institute of Standards and Technology specifically to evaluate the development of a fire and smoke transport. The simulation shows that CO2, as well as any smoke and combustion gases produced by a fire, would be discharged into the ISS cabin through the resource utility panel at the bottom of the rack. These simulations will be validated by comparing the results with velocity and CO2 concentration measurements obtained during the fire suppression system verification tests conducted on the CIR in March 2003. Once these numerical simulations are validated, portions of the ISS labs and living areas will be modeled to determine the local flow conditions before, during, and after a fire event. These simulations can yield specific information about how long it takes for smoke and combustion gases produced by a fire to reach a detector location, how large the fire would be when the detector alarms, and the behavior of the fire until it has been extinguished. This new capability could then be used to optimize the location of fire detectors and fire-suppression ports as well as to evaluate the effectiveness of fire suppressants and response strategies. Numerical data collected from these simulations could also be used to develop a virtual reality fire event for crew training and fire safety awareness. This work is funded by NASA's Bioastronautics Initiative, which has the objective of ensuring and enhancing the health, safety, and performance of humans in space. As part of this initiative, the Microgravity Combustion Science Branch at the NASA Glenn Research Center is conducting spacecraft fire safety research to significantly improve fire safety on inhabited spacecraft.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 185
    Publication Date: 2018-06-05
    Description: A fast-running unsteady aerodynamics code, LINFLUX, was previously developed for predicting turbomachinery flutter. This linearized code, based on a frequency domain method, models the effects of steady blade loading through a nonlinear steady flow field. The LINFLUX code, which is 6 to 7 times faster than the corresponding nonlinear time domain code, is suitable for use in the initial design phase. Earlier, this code was verified through application to a research fan, and it was shown that the predictions of work per cycle and flutter compared well with those from a nonlinear time-marching aeroelastic code, TURBO-AE. Now, the LINFLUX code has been applied to real configurations: fans developed under the Energy Efficient Engine (E-cubed) Program and the Quiet Aircraft Technology (QAT) project. The LINFLUX code starts with a steady nonlinear aerodynamic flow field and solves the unsteady linearized Euler equations to calculate the unsteady aerodynamic forces on the turbomachinery blades. First, a steady aerodynamic solution is computed for given operating conditions using the nonlinear unsteady aerodynamic code TURBO-AE. A blade vibration analysis is done to determine the frequencies and mode shapes of the vibrating blades, and an interface code is used to convert the steady aerodynamic solution to a form required by LINFLUX. A preprocessor is used to interpolate the mode shapes from the structural dynamics mesh onto the computational fluid dynamics mesh. Then, LINFLUX is used to calculate the unsteady aerodynamic pressure distribution for a given vibration mode, frequency, and interblade phase angle. Finally, a post-processor uses the unsteady pressures to calculate the generalized aerodynamic forces, eigenvalues, an esponse amplitudes. The eigenvalues determine the flutter frequency and damping. Results of flutter calculations from the LINFLUX code are presented for (1) the E-cubed fan developed under the E-cubed program and (2) the Quiet High Speed Fan (QHSF) developed under the Quiet Aircraft Technology project. The results are compared with those obtained from the TURBO-AE code. A graph of the work done per vibration cycle for the first vibration mode of the E-cubed fan is shown. It can be seen that the LINFLUX results show a very good comparison with TURBO-AE results over the entire range of interblade phase angle. The work done per vibration cycle for the first vibration mode of the QHSF fan is shown. Once again, the LINFLUX results compare very well with the results from the TURBOAE code.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 186
    Publication Date: 2018-06-05
    Description: A new in-house test capability has been developed at the NASA Glenn Research Center, where a critical component of the Stirling Radioisotope Generator (SRG) is undergoing extensive testing to aid the development of analytical life prediction methodology and to experimentally aid in verification of the flight-design component's life. The new facility includes two test rigs that are performing creep testing of the SRG heater head pressure vessel test articles at design temperature and with wall stresses ranging from operating level to seven times that (see the following photograph).
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 187
    Publication Date: 2018-06-05
    Description: The TopMaker technique was developed in an effort to reduce the time required for grid generation in complex numerical studies. Topology generation accounts for much of the man-hours required for structured multiblock grids. With regard to structured multiblock grids, topology refers to how the blocks are arranged and connected. A two-dimensional multiblock topology generation technique has been developed at the NASA Glenn Research Center. Very general configurations can be addressed by the technique. A configuration is defined by a collection of non-intersecting closed curves, which will be referred to as loops. More than a single loop implies that holes exist in the domain, which poses no problem. This technique requires only the medial vertices and the touch points that define each vertex. From the information about the medial vertices, the connectivity between medial vertices is generated. The physical shape of the medial edge is not required. By applying a few simple rules to each medial edge, a multiblock topology can be generated without user intervention. The resulting topologies contain only the level of complexity dictated by the configurations. Grid lines remain attached to the boundary except at sharp concave turns, where a change in index family is introduced as would be desired. Keeping grid lines attached to the boundary is especially important in computational fluid dynamics, where highly clustered grids are used near no-slip boundaries. This technique is simple and robust and can easily be incorporated into the overall grid-generation process.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research and Technology 2003; NASA/TM-2004-212729
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  • 188
    Publication Date: 2018-06-06
    Description: Over the past thirty years, numerical methods and simulation tools for incompressible flows have been advanced as a subset of the computational fluid dynamics (CFD) discipline. Although incompressible flows are encountered in many areas of engineering, simulation of compressible flow has been the major driver for developing computational algorithms and tools. This is probably due to the rather stringent requirements for predicting aerodynamic performance characteristics of flight vehicles, while flow devices involving low-speed or incompressible flow could be reasonably well designed without resorting to accurate numerical simulations. As flow devices are required to be more sophisticated and highly efficient CFD took become increasingly important in fluid engineering for incompressible and low-speed flow. This paper reviews some of the successes made possible by advances in computational technologies during the same period, and discusses some of the current challenges faced in computing incompressible flows.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 189
    Publication Date: 2018-06-06
    Description: Transport of solid-liquid slurries in pipeline transport over short and medium distances is very important in many industries, including mining related processes. The particle image velocimetry technique was successfully utilized to investigate the velocities and kinetic energy fluctuations of slurry particles at the tongue region of an optically-clear centrifugal pump. The experiments were conducted using 500 micron glass beads at volumetric Concentrations of 2.5% and 5% and at pump speeds of 725 rpm and 1000 rpm. The fluctuation kinetic energy increased approximately 200% to 500% as the pump speed was increased from 725 rpm to IO00 rpm. The directional impingement mechanism is more significant at the pressure side of the blade, tongue and the casing. This mechanism becomes more important as the speed increases. This suggests that the impeller; tongue and the casing of the slurry pump can wear out quickly, especially with an increase in speed. In this paper the emphasis is on the tongue region. The random impingement mechanism caused by the fluctuation kinetic energy of the solids can play an important role on the erosion of the tongue area.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Journal of Energy Resources Technology (ISSN 0195-0738); Volume 126; 271-278
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  • 190
    Publication Date: 2018-06-11
    Description: This Symposium is intended to bring together the often distinct cultures of the Stability and Control (S&C) community and the Computational Fluid Dynamics (CFD) community. The COMSAC program is itself a new effort by NASA Langley to accelerate the application of high end CFD methodologies to the demanding job of predicting stability and control characteristics of aircraft. This talk is intended to set the stage for needing a program like COMSAC. It is not intended to give details of the program itself. The topics include: 1) S&C Challenges; 2) Aero prediction methodology; 3) CFD applications; 4) NASA COMSAC planning; 5) Objectives of symposium; and 6) Closing remarks.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: COMSAC: Computational Methods for Stability and Control; 7-27; NASA/CP-2004-213028/PT1
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  • 191
    Publication Date: 2018-06-11
    Description: The motivation behind the inclusion of unsteady aerodynamics and aeroelastic effects in the computation of stability and control (S&C) derivatives will be discussed as they pertain to aeroelastic and aeroservoelastic analysis. This topic will be addressed in the context of two applications, the first being the estimation of S&C derivatives for a cable-mounted aeroservoelastic wind tunnel model tested in the NASA Langley Research Center (LaRC) Transonic Dynamics Tunnel (TDT). The second application will be the prediction of the nonlinear aeroservoelastic phenomenon known as Residual Pitch Oscillation (RPO) on the B-2 Bomber. Techniques and strategies used in these applications to compute S&C derivatives and perform flight simulations will be reviewed, and computational results will be presented.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: COMSAC: Computational Methods for Stability and Control, Part 2; 489-510; NASA/CP-2004-213028/PT2
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  • 192
    Publication Date: 2018-06-11
    Description: COMSAC goals include increasing the acceptance of CFD as a viable tool for S&C predictions, as well as to focus CFD development and improvement towards the needs of the S&C community. We view this as a symbiotic relationship, with increasing improvement of CFD promoting increasing acceptance by the S&C community, and increasing acceptance spurring further improvements. In this presentation we want to provide an overview for the non CFD expert of current CFD strengths and weaknesses, as well as to highlight a few emerging capabilities that we feel will lead toward increased usefulness in S&C applications.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: COMSAC: Computational Methods for Stability and Control; 48-68; NASA/CP-2004-213028/PT1
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  • 193
    Publication Date: 2019-07-18
    Description: Experiments have shown that moderate turbulence levels can nearly double turbine blade stagnation region heat transfer. Data have also shown that heat transfer is strongly affected by the scale of turbulence as well as its level. In addition to the stagnation region, turbulence is often seen to increase pressure surface heat transfer. This is especially evident at low to moderate Reynolds numbers. Vane and rotor stagnation region, and vane pressure surface heat transfer augmentation is often seen in a pre-transition environment. Accurate predictions of transition and relaminarization are critical to accurately predicting blade surface heat transfer. An approach is described which incorporates the effects of both turbulence level and scale into a CFD analysis. The model is derived from experimental data for cylindrical and elliptical leadng edges. Results using this model are compared to experimental data for both vane and rotor geometries. The comparisons are made to illustrate that using a model which includes the effects of turbulence length scale improves agreement with data, and to illustrate where improvements in the modeling are needed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Minnowbrook IV: 2003 Workshop on Transition and Unsteady Aspects of Turbomachinery Flows; 36; NASA/TM-2004-212913
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  • 194
    Publication Date: 2019-07-18
    Description: Computational Fluid Dynamics (CFD) is becoming an important component of injector design in the rocket industry. Injector designers who use CFD in the design process need to understand the accuracy level of the particular code being used for certain aspects of the design. This paper represents a recent effort to demonstrate the accuracy of two CFD codes to calculate the wall heat flux for a single element injector. The FDNS and Loci- CHEM codes currently in use at NASA Marshall Space Flight Center were evaluated. The test case was a single shear coaxial element with gaseous oxygen and hydrogen in a chamber instrumented with coaxial heat flux gauges on the chamber wall down the axis. The data were taken at Penn State University. Measured wall temperatures were used as boundary conditions for the CFD calculations. Calculations were compared to experimental data at chamber pressures of 300,450 600, and 750 psia. The accuracy level of both codes was assessed.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Jul 10, 2005 - Jul 13, 2005; Tucson, AZ; United States
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  • 195
    Publication Date: 2019-07-18
    Description: Solid-oxide fuel cells (SOFCs) show great potential as a power source for future space exploration missions. Because SOFCs operate at temperatures significantly higher than other types of fuel cells, they can reach overall efficiencies of up to 60% and are able to utilize fossil fuels. The SOFC team at GRC is leading NASA's effort to develop a solid oxide fuel cell with a power density high enough to be used for aeronautics and space applications, which is approximately ten times higher than ground transport targets. layers must be able to operate as a single unit at temperatures upwards of 900'C for at least 40,000 hours with less than ten percent degradation. One key challenge to meeting this goal arises from the thermal expansion mismatch between different layers. The amount a material expands upon heating is expressed by its coefficient of thermal expansion (CTE). If the CTEs of adjacent layers are substantially different, thermal stresses will arise during the cell's fabrication and operation. These stresses, accompanied by thermal cycling, can fracture and destroy the cell. While this is not an issue at the electrolyte-cathode interface, it is a major concern at the electrolyte-anode interface, especially in high power anode-supported systems. electrolyte are nearly identical. Conventionally, this has been accomplished by varying the composition of the anode to match the CTE of the yittria-stabilized zirconia (YSZ) electrolyte (approx.10.8x10(exp -6/degC). A Ni/YSZ composite is typically used as a base material for the anode due to its excellent electrochemical properties, but its CTE is about 13.4x10(exp -6/degC). One potential way to lower the CTE of this anode is to add a small percentage of polycrystalline Al2TiO5, with a CTE of 0.68x10(exp -6/degC, to the Ni/YSZ base. However, Al2TiO5 is thermally unstable and loses its effectiveness as it decomposes to Al2O3 and TiO2 between 750 C and 1280 C. be used as additives to increase the thermal stability of Al2TiO5 in SOFC operating conditions without adversely affecting the electrochemical properties of the SOFC anode. Three candidate materials were chosen through an extensive literature review: MgO, Fe2O3, and ZrTiO4. Although all three have been shown to prevent Al2TiO5 decomposition under various conditions, their effectiveness in the temperature range and atmosphere of the SOFC has not yet been evaluated. Several batches of Al2TiO5 with varying amounts of additives were prepared, exposed to reducing and oxidizing atmospheres at elevated temperatures, and the resulting decomposition of Al2TiO5 was measured. The most promising additives were further evaluated with the goal of ultimately preparing low CTE anodes that are chemically compatible to current systems. Adding minor constituents to stabilize Al2TiO5 could ultimately preserve its low CTE for the life of the fuel cell and improve the cell's long-term performance without a drop in anode conductivity. Further, these low CTE filler additions could allow the use of new sulfur tolerant anode materials, improving the viability of SOFCs for future aeronautics and space applications. Every SOFC consists of a cathode and an anode separated by an electrolyte, These three One way to avoid this problem is to design the cell such that the CTEs of the anode and The objective of this summer research project was to evaluate several materials that could
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Research Symposium II
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  • 196
    Publication Date: 2019-07-18
    Description: The density, viscosity, and electrical conductivity of Hg(sub 0.8)Cd(sub 0.2)Te melt were measures as a function of temperature. A pycnometric method was used to measure the melt density in the temperature range of 1072 to 1122 K. The viscosity and electrical conductivity were determined using a transient torque method from 1068 to 1132 K. The density result from this study is within 0.3% of the published data. However, the current viscosity result is approximately 30% lower than the existing data. The electrical conductivity of Hg(sub 0.8)Cd(sub 0.2)Te melt as a function of temperature, which is not available in the literature, is also determined. The analysis of the temperature dependent electrical conductivity and the relationship between the kinematic viscosity and density indicated that the structure of the melt appeared to be homogeneous when the temperature was above 1090 K. A structural transition occurred in the Hg(sub 0.8)Cd(sub 0.2)Te melt as the temperature was decreased to below 1090 K.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 197
    Publication Date: 2019-07-18
    Description: The relaxation phenomenon of semiconductor melts, or the change of melt structure with time, impacts the crystal growth process and the eventual quality of the crystal. The thermophysical properties of the melt are good indicators of such changes in melt structure. Also, thermophysical properties are essential to the accurate predication of the crystal growth process by computational modeling. Currently, the temperature dependent thermophysical property data for the Hg-based II-VI semiconductor melts are scarce. This paper reports the results on the temperature dependence of melt density, viscosity and electrical conductivity of Hg-based II-VI compounds. The melt density was measured using a pycnometric method, and the viscosity and electrical conductivity were measured by a transient torque method. Results were compared with available published data and showed good agreement. The implication of the structural changes at different temperature ranges was also studied and discussed.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 198
    Publication Date: 2019-07-18
    Description: New short-range order data are presented for equilibrium and undercooled liquids of Ti and Ni. These were obtained from in-situ synchrotron x-ray diffraction measurements of electrostatically-levitated droplets. While the short-range order of liquid Ni is icosahedral, consistent with Frank's hypothesis, significantly distorted icosahedral order is observed in liquid Ti. This is the first experimental observation of distorted icosahedral short-range order in any liquid. although this has been predicted by theoretical studies on atomic clusters.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 199
    Publication Date: 2019-07-18
    Description: The sedimentation dynamics of extremely low polydispersity, non-colloidal, particles are studied in a liquid fluidized bed at low Reynolds number, Re much less than 1. When fluidized, the system reaches a steady state, defined where the local average volume fraction does not vary in time. In steady state, the velocity fluctuations and the particle concentrations are found to strongly depend on height. Using our results, we test a recently developed stability model for steady state sedimentation. The model describes the data well, and shows that in steady state there is a balancing of particle fluxes due to the fluctuations and the concentration gradient. Some results are also presented for the dependence of the concentration gradient in fluidized beds on particle size; the gradients become smaller as the particles become larger and fewer in number.
    Keywords: Fluid Mechanics and Thermodynamics
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  • 200
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    In:  Other Sources
    Publication Date: 2019-07-18
    Description: In the past we have used thermal imaging techniques to visualize the cryocooling processes of macromolecular crystals. From these images it was clear that a cold wave progresses through a crystal starting at the face closest to the origin of the cold stream and ending at the point furthest away. During these studies we used large volume crystals, which were clearly distinguished fiom the loop holding them. These large crystals, originally grown for neutron diffiaction studies, were chosen deliberately to enhance the imaging. As an extension to this work, we present used thermal imaging to study small crystals, held in a cryo-loop, in the presence of vitrified mother liquor. The different d a r e d transmission and reflectance properties of the crystal in comparison to the mother liquor surrounding it are thought to be the parameter that produces the contrast that makes the crystal visible. An application of this technology may be the determination of the exact location of small crystals in a cryo-loop. Data fkom initial tests in support of application development was recorded for lysozyme crystals and for bFGF/dna complex crystals, which were cryocooled and imaged in large loops, both with visible light mad with h i k e d rdi&tion. The crystals were clearly distinguished from the vitrified solution in the infiared spectrum, while in the case of the bFGF/dna complex the illumination had to be carefully manipulated to make the crystal visible in the visible spectrum. These results suggest that the thermal imaging may be more sensitive than visual imaging for automated location of small crystals. However, further work on small crystals robotically mounted at SSRL did not clearly visualize those crystals. The depth of field of the camera proved to be limiting and a different cooling geometry was used, compared to the previous, successful experiments. Analysis to exploit multiple images to improve depth of field and experimental work to understand cooling geometry effects is ongoing. These results will be presented along with advantages and disadvantages of the technique and a discussion of how it might be applied.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Hauptmann Woodward Medical Research Institute Meeting; Apr 26, 2004; Buffalo, NY; United States
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