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  • Other Sources  (457)
  • FLUID MECHANICS AND HEAT TRANSFER  (225)
  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (171)
  • Inorganic Chemistry
  • Seismology
  • 1980-1984  (457)
  • 1955-1959
  • 1981  (457)
Collection
Years
  • 1980-1984  (457)
  • 1955-1959
Year
  • 1
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    In:  Rev. Geophys. Space Phys., Taipei, Elsevier, vol. 19, no. B2, pp. 649-663, pp. B02317, (ISBN: 0-12-018847-3)
    Publication Date: 1981
    Keywords: Seismology ; Scaling ; Magnitude ; Nuclear explosion
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  • 2
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    In:  Geophys. J. R. astr. Soc., Warszawa, Army Corps of Engineers, Woodward-Clyde Consultants, vol. 67, no. 36, pp. 375-393, pp. B05310, (ISBN: 0-12-018847-3)
    Publication Date: 1981
    Keywords: Source ; Seismology ; Fracture ; GJRaS
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  • 3
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    In:  J. Geophys. Res., Warszawa, Army Corps of Engineers, Woodward-Clyde Consultants, vol. 86, no. 36, pp. 6039-6051, pp. B05310, (ISBN: 0-12-018847-3)
    Publication Date: 1981
    Keywords: Friction ; Fracture ; Rock mechanics ; Seismology ; JGR
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  • 4
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    In:  Phys. Earth Planet. Inter., Luxembourg, U.S. Geological Survey, vol. 25, no. 24, pp. 297-356, pp. B05309, (ISBN 0-471-26610-8)
    Publication Date: 1981
    Keywords: Seismology ; Earth model, also for more shallow analyses ! ; PREM ; PEPI ; Dziewonski
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  • 5
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    In:  Rev. Roum. Géol., Géophys. et Géogr. - Géophysique, Münster, 3, vol. 25, no. 3-4, pp. 17-34, pp. L12311, (ISBN 0-471-26610-8)
    Publication Date: 1981
    Keywords: Earthquake ; Seismology ; EUROPROBE (Geol. and Geophys. in eastern Europe) ; Fault plane solution, focal mechanism
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  • 6
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    In:  Bull. Seism. Soc. Am., Luxembourg, Conseil de l'Europe, vol. 71, no. 7055, pp. 2071-2095, pp. B05S07, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1981
    Keywords: Seismology ; Strong motions ; Spectrum ; BSSA
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  • 7
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    In:  Bull. seism. Soc. Am., Helsinki, Icelandic Meteorological Office, Ministry for the Environment University of Iceland, vol. 71, no. 2, pp. 1763-1781, pp. 2265, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1981
    Keywords: SH waves ; Layers ; Seismology ; NOModelling ; Synthetic seismograms ; BSSA
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  • 8
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    In:  Int. J. Rock Mech. Min. Sci. & Geomech. Abstr., San Francisco, Pergamon, vol. 18, no. 8, pp. 517-527, pp. 1121, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Energy (of earthquakes) ; nuclear ; waste ; disposal
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  • 9
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    In:  J. Geophys. Res., New York, August, vol. 86, no. 3-4, pp. 3901-3912, pp. 1610, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Strong motions ; Seismology ; Inhomogeneity ; Fracture ; JGR
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  • 10
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    In:  Bull. Seism. Soc. Am., New York, August, vol. 71, no. 3-4, pp. 1061-1074, pp. B05S05, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: earth mantle ; Seismology ; P-waves ; residues ; BSSA
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  • 11
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    In:  Bull. Seism. Soc. Am., (submitted), Icelandic Meteorological Office, Ministry for the Environment University of Iceland, vol. 71, no. 1-2, pp. 2011-2038, pp. TC1011, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1981
    Keywords: Seismology ; Strong motions ; Earthquake ; BSSA
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  • 12
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    In:  J. Phys. Earth, Bonn, 3-4, vol. 29, no. 1, pp. 221-239, pp. B01401, (ISSN: 1340-4202)
    Publication Date: 1981
    Description: Ellipsoid-Least-Squares-Fit
    Keywords: Seismology ; Polarization ; Three component data ; JPE
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  • 13
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    In:  Geol. Jb., Würzburg, Physica-Verlag, vol. E21, no. 1, pp. 13-25, pp. L24313, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: P-waves ; Fracture ; Fracture time (duration) ; Earthquake ; Seismology ; Seismic arrays
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  • 14
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    In:  Bull. Seism. Soc. Am., Basel, Elsevier Science Publishers, vol. 71, no. 8, pp. 1-24, pp. L15S20, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Earthquake ; Inversion ; Source parameters ; BSSA
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  • 15
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    In:  J. Geophys. Res., Luxembourg, EGS-Gauthier-Villars, vol. 86, no. 1-4, pp. 10821-10834, pp. L23608
    Publication Date: 1981
    Keywords: Seismology ; Source parameters ; Statistical investigations ; Fault zone ; JGR
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  • 16
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    In:  Geophys. J. R. astr. Soc., Münster, 3, vol. 66, no. 2, pp. 37-69, pp. L23301, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1981
    Keywords: NOModelling ; Layers ; Seismology ; Synthetic seismograms ; GJRaS
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  • 17
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    In:  J. Geophys. Res., Oslo, Wiley, vol. 86, no. 2, pp. 5963-5984, pp. L02304, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Moment tensor ; Inversion ; Seismicity ; Rayleigh waves ; Phase velocity ; Hypocentral depth ; JGR
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  • 18
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    In:  Geophysics, Basel, Inst. f. Geophys., Ruhr-Univ. Bochum, vol. 46, no. 3, pp. 1423-1431, pp. 1009, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Seismics (controlled source seismology) ; Filter- ; Polarization
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  • 19
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    In:  Earthquake Notes, Luxembourg, Conseil de l'Europe, vol. 51, no. 3, pp. 71, pp. 1006, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Earthquake ; Source
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  • 20
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    In:  J. Geophys. Res., Luxembourg, Conseil de l'Europe, vol. 86, no. 1-4, pp. 7874-7894, pp. 1006, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Earthquake ; Seismology ; Geol. aspects ; Tectonics ; JGR
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  • 21
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    In:  J. Geophys., Luxembourg, Deutsche Geophys. Gesellschaft, vol. 49, no. 2, pp. 243-244, pp. 8045, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismicity ; Seismology ; Detectors ; Kulhanek ; Wahlstroem ; Wahlstrom
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  • 22
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    In:  Bull. Earthq. Res. Inst., Corvallis, x + 406 pp., Oregon State University Press, vol. 55, no. 1-4, pp. 449-484, pp. L13610, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Travel time ; Data analysis / ~ processing
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  • 23
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    D. Reidel Publ. Comp.
    In:  London, D. Reidel Publ. Comp., vol. special paper 359, ix + 190 pp., no. 2, pp. 497-504, (ISBN 0-8137-2359-0)
    Publication Date: 1981
    Keywords: Discrimination ; Seismology ; ConvolutionR ; Source ; Nuclear explosion
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  • 24
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    Academic Press
    In:  New York, 293 pp., Academic Press, vol. 34, no. 22, pp. 65-70, (ISBN 0-691-12183-4, 2005 (481 pp. + CD-ROM))
    Publication Date: 1981
    Keywords: Seismic networks ; Handbook of geophysics ; Seismology
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  • 25
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    Am. Geophys. Un.
    In:  Professional Paper, Zagros, Hindu Kush, Himalaya: Geodynamic Evolution, Washington, D. C., Am. Geophys. Un., vol. 65, no. 16, pp. 243-271, (ISBN 1-86239-165-3, vi + 330 pp.)
    Publication Date: 1981
    Keywords: Fault plane solution, focal mechanism ; Tectonics ; Plate tectonics ; Seismology
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  • 26
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    In:  Earth-Sci. Rev., Ottawa, Bundesanstalt für Geowissenschaften und Rohstoffe, vol. 17, no. 3-4, pp. 315-398, pp. L14310
    Publication Date: 1981
    Keywords: Magnitude ; Seismology ; Review article ; Bath
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  • 27
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    In:  Acta Seismologica Sinica, Tokyo, Terra Scientific Publishing Company, vol. 3, no. 1-3, pp. 335-350, pp. B05S09, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1981
    Keywords: Surface waves ; CRUST ; China ; Seismology ; Seismics (controlled source seismology)
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  • 28
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    In:  J. Geophys. Res., Tokyo, Terra Scientific Publishing Company, vol. 86, no. 8, pp. 9357-9374, pp. B05S21, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1981
    Keywords: Seismology ; Moment tensor ; Source parameters ; Earthquake ; Hypocentral depth ; JGR
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  • 29
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    In:  Bull. Seism. Soc. Am., Bonn, Pergamon, vol. 71, no. 4, pp. 1351-1360, pp. 2050, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1981
    Keywords: Seismology ; Detectors ; sta ; Transformations ; squ ; median ; BSSA
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  • 30
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    In:  Phys. Earth Plan. Int., vol. 27, no. 1-4, pp. 72-92
    Publication Date: 1981
    Keywords: Magnitude ; Seismology ; Earthquake catalog ; PEPI
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  • 31
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    In:  Bull. seism. Soc. Am., Taipei, Elsevier, vol. 71, no. 2, pp. 161-181, pp. B09401, (ISBN: 0-12-018847-3)
    Publication Date: 1981
    Keywords: Attenuation ; Surface waves ; NOModelling ; CRUST ; Seismology ; Quality factor ; BSSA
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  • 32
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    Polish Academy of Sciences
    In:  Publications of the Institute of Geophysics, Warszawa, Polish Academy of Sciences, vol. A-11(147), no. 18, pp. 16-1 to 16-4, pp. 1869, (ISBN: 0-12-018847-3)
    Publication Date: 1981
    Keywords: Seismology ; Source parameters ; Inversion ; Induced seismicity ; Mining geophysics
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  • 33
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    In:  J. Geophys. Res., Luxembourg, U.S. Geological Survey, vol. 86, no. 3-4, pp. 2825-2852, pp. B05309, (ISBN 0-471-26610-8)
    Publication Date: 1981
    Keywords: Source parameters ; Seismology ; Source ; Seismicity ; Wave form analysis ; JGR ; Dziewonski
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  • 34
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    In:  Geophys. J. R. astr. Soc., Dordrecht, National Academy of Sciences of the USA, vol. 64, no. 5-6, pp. 605-634, pp. TC5003, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: NOModelling ; Inhomogeneity ; Seismology ; GJRaS
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  • 35
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    In:  Bull. Seism. Soc. Am., Washington, D.C., AGU, vol. 71, no. B12, pp. 1701-1718, pp. B12406, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Broad-band ; Earthquake ; BSSA
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  • 36
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    Springer
    In:  New York, 1108 pp., Springer, vol. 96, pp. 225, (ISBN 0-471-95596-5)
    Publication Date: 1981
    Keywords: FROTH ; RUB ; GMG ; 3.15.80 ; Textbook of geophysics ; Seismology ; Waves ; Wavelet processing ; SModelling ; Dislocation ; Elasticity theory of dislocations ; Source
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  • 37
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    Reidel
    In:  Amsterdam, Reidel, vol. 65, no. XVI:, pp. 1-14, (ISBN 0-521-80380-2 (hb), 0521-00859-X (pb))
    Publication Date: 1981
    Keywords: Nuclear explosion ; Seismology ; Discrimination ; Source
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  • 38
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    Cambridge Univ. Press
    In:  Cambridge, XIII+248 pp., Cambridge Univ. Press, vol. 7, no. XVI:, pp. 227-235, (ISBN 0231-12739-1 hb, 0231127383 pb)
    Publication Date: 1981
    Keywords: Seismology ; Earthquake ; Textbook of geophysics
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  • 39
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    AGU
    In:  Washington, D.C., AGU, vol. 4, no. Publ. No. 12, pp. 9, (3-540-24165-5, XXVI + 228 p.)
    Publication Date: 1981
    Keywords: Handbook of geophysics ; Earthquake precursor: prediction research ; Earthquake precursor: deformation or strain ; Seismicity ; Seismology
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  • 40
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    In:  Geophys. Res. Lett., Tokyo, Railway Tech. Res. Inst., vol. 8, no. 12, pp. 33-35, pp. B06403, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Seismics (controlled source seismology) ; CRUST ; earth mantle ; Travel time ; GRL ; Necioglu
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  • 41
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    Czechoslovak Academy of Sciences
    In:  Proceedings, 1., Prag, Czechoslovak Academy of Sciences, vol. 10, no. WS-693 7-83, pp. 235-239, (ISBN 3-933346-037)
    Publication Date: 1981
    Keywords: Seismology ; Seismicity ; Earthquake precursor: prediction research ; Earthquake risk ; Earthquake hazard ; Proceedings of a conference
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  • 42
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    In:  J. Geophys. Res., Washington, D.C., AGU, vol. 86, no. B12, pp. 1679-1685, pp. B12406, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Source parameters ; Inversion ; JGR
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  • 43
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    In:  Nature, Reykjavík, Icelandic Meteorological Office, Ministry for the Environment, University of Iceland, vol. 289, no. 11, pp. 785-787, pp. L05306, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismicity ; Earthquake precursor: statistical anal. of seismicity ; Seismology ; Earthquake precursor: prediction research ; FROTH ; (abstract)
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  • 44
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    D. Reidel Publishing Company
    In:  Professional Paper, Identification of Seismic Sources - Earthquake or Underground Explosion, Berlin, D. Reidel Publishing Company, vol. 24, no. 16, pp. 695-740, (ISBN 0080419208)
    Publication Date: 1981
    Keywords: Seismology ; Nuclear explosion ; Discrimination
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  • 45
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    Reidel
    In:  Bull., Polar Proj. OP-O3A4, Current Research in Earthquake Prediction, Dordrecht, Reidel, vol. I, no. XVI:, pp. 221-300, (ISBN: 3-540-23712-7)
    Publication Date: 1981
    Keywords: Earthquake precursor: prediction research ; Seismicity ; Seismology ; Earthquake precursor: stresses ; Fault plane solution, focal mechanism
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  • 46
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    In:  Bull., Polar Proj. OP-O3A4, Identification of Seismic Sources - Earthquake or Underground Explosion, Leiden, Noordhoff, vol. 11, no. XVI:, pp. 763-786, (ISBN: 3-540-23712-7)
    Publication Date: 1981
    Keywords: Seismology ; Broad-band ; Seismic arrays ; Data analysis / ~ processing ; Nuclear explosion ; Review article
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  • 47
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    D. Reidel Publ. Co.
    In:  Bull., Polar Proj. OP-O3A4, Identification of Seismic Sources - Earthquake or Underground Explosion, Moscow, D. Reidel Publ. Co., vol. 65, no. Subvol. a, pp. 467-481, (ISBN 0080419208)
    Publication Date: 1981
    Keywords: Seismology ; NOR ; PIC ; f-k-Analysis ; Seismic arrays ; NOISE ; AUD ; Location ; Nuclear explosion
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  • 48
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    In:  J. Volcanol. Geotherm. Res., Kyoto, AGU, vol. 9, no. 6, pp. 311-344, pp. L24617, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Earthquake ; Source
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  • 49
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    In:  Umschau, New York, Scientific American, vol. 81, no. B9, pp. 443, pp. B09309, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismic arrays ; Seismology
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  • 50
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    In:  Bull. Seism. Soc. Am., Kunming, China, AGU, vol. 71, no. 5636, pp. 1883-1902, pp. L14317, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Review article ; Seismicity ; Source parameters ; Seismology ; BSSA
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  • 51
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    William Kaufmann, Inc.
    In:  Los Altos, California, William Kaufmann, Inc., vol. Developments in Petroleum Science vol. 15B, no. Publ. No. 12, pp. 9, (3-540-24165-5, XXVI + 228 p.)
    Publication Date: 1981
    Keywords: Seismology ; Handbook of geophysics
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  • 52
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    Czechoslovak Academy of Sciences
    In:  Proceedings, 2., Prag, Czechoslovak Academy of Sciences, vol. 10, no. WS-693 7-83, pp. 235-239, (ISBN 3-933346-037)
    Publication Date: 1981
    Keywords: Seismology ; Seismicity ; Earthquake precursor: prediction research ; Earthquake risk ; Earthquake hazard ; Proceedings of a conference
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  • 53
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    Geophysikalisches Inst.
    In:  Diplomarbeit, Univ. Karlsruhe, Geophysikalisches Inst., vol. 1034, no. 77-3, pp. 262-277, (ISBN 3-933346-037)
    Publication Date: 1981
    Keywords: Seismology ; seismic Moment ; Earthquake ; Synthetic seismograms ; Rakers
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  • 54
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    Lawrence Livermore National Laboratory
    In:  informal report, Houston, Lawrence Livermore National Laboratory, vol. 339-350, no. UCID-18928, pp. 344, (ISBN 3-933346-037)
    Publication Date: 1981
    Keywords: Seismology ; Nuclear explosion ; NOISE ; Spectrum ; Geol. aspects ; Seismicity
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  • 55
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    In:  Houston, no. 18, pp. 143-179
    Publication Date: 1981
    Keywords: Seismology ; Statistical investigations ; Inhomogeneity
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  • 56
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    In:  Tectonophysics, Dordrecht, Martinus Nijhoff Publishers, vol. 72, no. 5705, pp. 181-201, pp. 2389, (ISSN: 1340-4202)
    Publication Date: 1981
    Keywords: Seismology ; Inelastic ; Attenuation ; Elasticity ; earth mantle
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  • 57
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    In:  Bull. Seism. Soc. Am., Zagreb, Conseil de l'Europe, vol. 71, no. 4, pp. 731-745, pp. L02307, (ISSN 0343-5164)
    Publication Date: 1981
    Keywords: Seismology ; Earthquake ; Earthquake catalog ; BSSA
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  • 58
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    In:  Bull. Seism. Soc. Am., Zagreb, Conseil de l'Europe, vol. 71, no. 4, pp. 1963-1979, pp. L02307, (ISSN 0343-5164)
    Publication Date: 1981
    Keywords: Seismology ; Strong motions ; BSSA
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  • 59
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    Universität Karlsruhe
    In:  Dissertation, Grenoble, Universität Karlsruhe, vol. 10, no. GL-TR-89-0230, pp. 95-134, (ISBN 3-933346-037)
    Publication Date: 1981
    Keywords: Seismology ; PKP ; earth Core ; Earth model, also for more shallow analyses ! ; Velocity depth profile ; Synthetic seismograms ; Transformations ; Hage
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  • 60
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    VELA Seismological Center
    In:  report, Arlington, Virginia, VELA Seismological Center, vol. 10, no. VSC-TR-81-19, pp. 484-486, (ISBN 3-933346-037)
    Publication Date: 1981
    Description: Polar. filter (von Smart, 1977) zur Detektion u Bestimmung des Azimuts, Anwendung auf P und Lg-Phasen in kurz-periodischen Daten der Station RKON. unterschiedlich zitiert bei Christ. und ...
    Keywords: Seismology ; Data analysis / ~ processing ; Filter- ; Detectors ; Polarization
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  • 61
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    Inst. of Geophys., Univ. Frankfurt
    In:  Reisebericht an die Max-Planck-Gesellschaft, Bad Bergzabern, Inst. of Geophys., Univ. Frankfurt, vol. 10, no. 13, pp. 1-217
    Publication Date: 1981
    Keywords: Seismology ; Earthquake precursor: prediction research ; Project report/description
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  • 62
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    In:  CASI
    Publication Date: 2006-02-14
    Description: As a part of the EET aerodynamics program an out-of-house program was developed and monitored to provide theoretical procedures useful in the design of transport aircraft. The focus of the effort was to provide tools valid in the nonlinear transonic speed range. The effort was divided into two basic areas, inviscid configuration analysis and design procedures and viscous correction procedures.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Advan. Aerodyn.: Selected NASA Res.; p 79-94
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  • 63
    Publication Date: 2006-02-14
    Description: Improvements in cruise efficiency on the order of 15 to 40% are obtained by increasing the extent of laminar flow over lifting surfaces. Two methods of achieving laminar flow are being considered, natural laminar flow and laminar flow control. Natural laminar flow (NLF) relies primarily on airfoil shape while laminar flow control involves boundary layer suction or blowing with mechanical devices. The extent of natural laminar flow that could be achieved with consistency in a real flight environment at chord Reynolds numbers in the range of 30 x 10(6) power was evaluated. Nineteen flights were conducted on the F-111 TACT airplane having a NLF airfoil glove section. The section consists of a supercritical airfoil providing favorable pressure gradients over extensive portions of the upper and lower surfaces of the wing. Boundary layer measurements were obtained over a range of wing leading edge sweep angles at Mach numbers from 0.80 to 0.85. Data were obtained for natural transition and for a range of forced transition locations over the test airfoil.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Langley Research Center Advan. Aerodyn.: Selected NASA Res.; p 11-20
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  • 64
    Publication Date: 2006-02-14
    Description: Anchorage dependent cell cultures in fluidized beds are tested. Feasibility calculations indicate the allowed parameters and estimate the shear stresses therein. In addition, the diffusion equation with first order reaction is solved for the spherical shell (double bubble) reactor with various constraints.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Houston Univ. The 1981 NASA ASEE Summer Fac. Fellowship Program, Vol. 2; 19 p
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  • 65
    Publication Date: 2006-02-14
    Description: Technical improvements of a long life heat rejection system, suitable for long duration high power missions, that can be constructed and deployed in orbit is discussed. A mathematical model is formulated and a computer program developed which describes the transient priming characteristics of a dual passage heat pipe. An experimental test package is described for flight in the KC-135 Zero-g Aircraft, to be used to verify the modeling predictions.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Houston Univ. The 1981 NASA ASEE Summer Fac. Fellowship Program, Vol. 2; 50 p
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  • 66
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    In:  CASI
    Publication Date: 2006-02-14
    Description: A summary on heavy rain effects on aircraft aerodynamics validation of research and some wind shear accidents in which heavy rain were an important factor. Frost formation and what frost does to the lift and drag curves for an airfoil was examined. If frost could cause severe aerodynamic problems for both general aviation and transport aircraft due to its roughness, then heavy rain produce a similar result. The influencing parameters of heavy rain on an aircraft are studied. Sources of aerodynamic roughness due to rain and wind shear and heavy rain accidents are outlined.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Marshall Space Flight Center Proc.: 5th Ann. Workshop on Meteorol. and Environ. Inputs to Aviation Systems 76-80 (SEE N82-21139 12-01)
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  • 67
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    In:  CASI
    Publication Date: 2006-02-14
    Description: Meteorology impact on future aircraft design is discussed. Upcoming changes in both design and operations that will be influenced by the meteorological environment are outlined. Future and more nonconventional designs and meteorological impact brought about by operational changes over the next few years are examined.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Marshall Space Flight Center Proc.: 5th Ann. Workshop on Meteorol. and Environ. Inputs to Aviation Systems; p 29-34
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  • 68
    Publication Date: 2006-02-14
    Description: The connection between fuel consumption and weather data is discussed. Fuel efficient flights creating adequate near real time weather information are examined. The lack of highly resolved real time and near real time wind and temperature data at flight altitudes is investigated. The existing systems, which is based on twice a day balloon observations, supplemented by pilot reports or other occasional data, is not adequate for optimum flight planning. The impacts of upper winds and temperatures on fuel efficiency and flight planning are not widely appreciated and developing new weather products are considered.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Marshall Space Flight Center Proc.: 5th Ann. Workshop on Meteorol. and Environ. Inputs to Aviation Systems; p 15-19
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  • 69
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    In:  CASI
    Publication Date: 2006-02-14
    Description: Spacelab experiment to investigate two-phase flow patterns under gravity uses a water-air mixture experiment. Air and water are circulated through the system. The quality or the mixture or air-water is controlled. Photographs of the test section are made and at the same time pressure drop across the test section is measured. The data establishes a flow regime map under reduced gravity conditions with corresponding pressure drop correlations. The test section is also equipped with an electrical resistance heater in order to allow a flow boiling experiment to be carried out using Freon II. High-speed photographs of the test section are used to determine flow patterns. The temperature gradient and pressure drop along the duct can be measured. Thus, quality change can be measured, and heat transfer calculated.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 43-57
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  • 70
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    In:  CASI
    Publication Date: 2006-02-14
    Description: The equations of motion governing an incompressible fluid contained in an orbiting laboratory were examined to isolate various fictitious forces and their relative influence on the fluid. The forces are divided into those arising from the orbital motions and those arising from small local motions of the spacecraft about its center of mass. The latter dominate the nonrotating experiments. Both are important for rotating experiments. A brief discussion of the onset of time-dependence and violent instability in earth-based rotating and processing systems is given.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 96-102
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  • 71
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    In:  CASI
    Publication Date: 2006-02-14
    Description: Natural convection is not always harmful and, therefore, to be avoided. In some situations it may be desirable to have fluid flows in space processes, e.g., to stir the fluid phase for mixing and cooling or to help maintain concentration gradients. In may event, it is important to know the extent and nature of convection in space and the factors on which it depends, in order either to minimize the effects to convection, or to utilize the convection to advantage. The information needed to assess both conventional and unstable convection includes: (1) the magnitude and direction of accelerations; (2) geometric configuration; (3) imposed boundary conditions; and (4) material properties.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA. Marshall Space Flight Center Spacecraft Dyn. as Related to Lab. Expt. in Space; p 69-95
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  • 72
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    In:  CASI
    Publication Date: 2006-02-14
    Description: Systematic scaling or dimensional analysis reveals that certain scales of geophysical fluid flows (such as stellar, ocean, and planetary atmosphere circulations) can be accurately modeled in the laboratory using a procedure which differs from conventional engineering modeling. Rather than building a model to obtain numbers for a specific design problem, the relative effects of the significant forces are systematically varied in an attempt to deepen understanding of the effects of these forces. Topics covered include: (1) modeling a large-scale planetary atmospheric flow in a rotating cylindrical annulus; (2) achieving a radial dielectric body force; (3) spherical geophysical fluid dynamics experiments for Spacelab flights; (4) measuring flow and temperature; and (5) the possible effect of rotational or precessional disturbances on the flow in the rotating spherical containers.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Spacecraft Dyn. as Related to Lab. Expt. in Space; p 25-31
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  • 73
    Publication Date: 2006-02-14
    Description: After the external tank separates from the Orbiter about 2000 pounds of residual liquid oxygen remain in the main propulsion system lines. The pressurization of liquid oxygen from a subcritical to a supercritical state by the use of the heaters of the PRSA tanks while in a low-g environment is investigated. The performance of the heaters while bringing the state of the substance from the subcritical state to the supercritical one is studied, with particular emphasis on the time the pressurization process takes, and the temperature of the heater as the process proceeds.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Houston Univ. The 1981 NASA ASEE Summer Fac. Fellowship Program, Vol. 2; 38 p
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  • 74
    Publication Date: 2011-08-18
    Description: The problem of forced fluid vibrations in a partially filled spinning spherical tank is solved numerically by using the finite element method. The governing equations include Coriolis acceleration and spatially homogeneous vorticity. An exponential instability is detected in the present simulation for fill ratios below 0.5 and centrifugal acceleration to thrust ratios less than 1.7. This fictitious instability appears in the model as a result of the homogeneous vortex assumption since the free slosh equations are neutrally stable in the Liapunov sense.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Sound and Vibration; 76; May 8
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  • 75
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    Publication Date: 2011-08-18
    Description: The use and modifications of the T-38 aircraft as chase planes for the STS-1 landing are discussed. Two planes tracked the approach at Edwards AFB, with the lead plane responsible for airspeed and altimetry calibration, technical photography, landing gear status, and height-above-touchdown calls; the second T-38 provided live TV and back-up. Modifications included extension of the landing gear extension speed, increasing the area of the speedbrakes, and installation of a TV system; the goal was to stay with the Shuttle below 40,000 ft while it descended at 15,000 ft/min. Ten T-38's were modified and the deployment of lead and back-up crews during the first Shuttle flight is outlined. Western Test Range C-band radar data of the Orbiter position were transformed into intercept coordinates and VHF relayed to the chase craft. Photographs were taken of the right and left sides and underside of the Shuttle while flying with the speedbrake up to match the Shuttle speed.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
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  • 76
    Publication Date: 2011-08-18
    Description: Heat transfer characteristics are analyzed for a cooled two-dimensional porous medium having a curved boundary. A general analytical procedure is given in combination with a numerical conformal mapping method used to transform the porous region into an upper half plane. To illustrate the method, results are evaluated for a cosine shaped boundary subjected to uniform external heating. The results show the effects of coolant starvation in the thick regions of the medium, and the extent that internal heat conduction causes the heated surface to have a more uniform temperature.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
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  • 77
    Publication Date: 2011-08-18
    Description: The development of a comprehensive analytical model of rotorcraft aerodynamics and dynamics is described. Particular emphasis is given to describing the reasons behind the choices and decisions involved in constructing the model. The analysis is designed to calculate rotor performance, loads and noise; helicopter vibration and gust response; flight dynamics and handling qualities; and system aeroelastic stability. It is intended for use in the design, testing and evaluation of a wide class of rotors and rotorcraft and to be the basis for further development of rotary wing theories. The general characteristics of the geometric, structural, inertial and aerodynamic models used for the rotorcraft components are described, including the assumptions introduced by the chosen models and the resulting capabilities and limitations. Finally, some examples from recent applications of the analysis are given.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Vertica; 5; 3, 19; 1981
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  • 78
    Publication Date: 2011-08-18
    Description: An interactive method is proposed for the solution of two-dimensional, laminar flow fields with identifiable regions of recirculation, such as the shear-layer-driven cavity flow. The method treats the flow field as composed of two regions, with an appropriate mathematical model adopted for each region. The shear layer is computed by the compressible boundary layer equations, and the slowly recirculating flow by the incompressible Navier-Stokes equations. The flow field is solved iteratively by matching the local solutions in the two regions. For this purpose a new matching method utilizing an overlap between the two computational regions is developed, and shown to be most satisfactory. Matching of the two velocity components, as well as the change in velocity with respect to depth is amply accomplished using the present approach, and the stagnation points corresponding to separation and reattachment of the dividing streamline are computed as part of the interactive solution. The interactive method is applied to the test problem of a shear layer driven cavity. The computational results are used to show the validity and applicability of the present approach.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Computational Physics; 40; Apr. 198
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  • 79
    Publication Date: 2011-08-18
    Description: The shear-free turbulent boundary layer is calculated by the large-eddy simulation technique. The filtered Navier-Stokes equations are used; the method of integration employs Fourier expansions in the homogeneous directions and finite differences in the cross-stream direction. Results indicate that the simulation is capable of predicting the primary Reynolds-number effects.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Fluid Mechanics; 103; Feb. 198
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  • 80
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    Publication Date: 2011-08-18
    Description: Action to be taken to prepare to implement efficient, modern commuter aircraft for the 1990s is outlined. The increase in the contribution of jet fuel costs to aircraft direct operating costs (DOC) is noted as the motivation for the introduction of turboprop-powered commuter aircraft, which use 15-20% less fuel per seat mile at short stage lengths, to replace larger jet transports. Designs proposed by various manufacturers which will make use of existing technology for 19-, 30- and 50-seat aircraft capable of carrying a full payload of passengers and baggage for 600 n mi and optimized for minimum DOC over a 100-n mi stage length are presented, and the improvements in fuel usage, DOC and passenger comfort to be obtained with the use of advanced technology are pointed out. The goals and considered technologies of the dedicated small-transport aircraft technology program recommended by a commuter air transport subcommittee of the NASA Advisory Council Aeronautics Advisory Committee to speed the development of commuter technology are then presented, with attention given to efforts of analysis, design and testing of propulsion systems, structures, aerodynamics and systems intended to result in 16-24% savings in DOC and up to 40% savings in fuel. The commuter development plans of various manufacturers are also indicated.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Astronautics and Aeronautics; 19; Feb. 198
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  • 81
    Publication Date: 2011-08-18
    Description: The quantum mechanical technique is used to study ionic, configurational, and impurity defects in the ice surface. In addition to static calculations of the energetics of the water monomer-ice surface interactions, molecular dynamics studies were initiated. The calculations of the monomer-ice surface interaction, molecular dynamics studies were initiated. The calculations of monomer-ice surface interactions indicate that many adsorption sites exist on the ice surfaces and that the barriers between bonding sites are relatively low. Bonding on the prism face of ice is preferentially above lattice sites.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: A Mol. Model for Ice Nucleation and Growth; 27 p
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  • 82
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    Publication Date: 2011-08-18
    Description: The central field empirical pair potential model is applied to studying the effects of kinks, ledges, and vacancies on the absorption of water molecules from the vapor. Molecular dynamics simulations indicate that cluster and/or surface modes play a primary role in the absorption process, the flexibility of the hydrogen bond serves to decrease the energy required for structural interconversion, and the rapid distribution of added energy in a hydrogen bonded system lead to aggregate stability which greatly exceeds that predicted by static energy calculations.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: A Mol. Model for Ice Nucleation and Growth; 22 p
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  • 83
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    Publication Date: 2011-08-18
    Description: Areas of investigation in fluid dynamics, recommended experiments, and use of the facility for theory evaluation are discussed. Tunnel flow quality and calibration of the NTF are considered. Recent technological advances affecting tunnel design are surveyed.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: High Reynolds Number Res. - 1980; p 169-195
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  • 84
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    Publication Date: 2011-08-18
    Description: The aerodynamic characteristics which affect the fuel consumption of general aviation aircraft are outlined. All data are presented in the form of graphs.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Langley Research Center Joint Univ. Program for Air Transportation Res., 1980; p 133-142
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  • 85
    Publication Date: 2011-08-18
    Description: The conservation-law form of the inviscid gasdynamic equations has the remarkable property that the nonlinear flux vectors are homogeneous functions of degree one. This property readily permits the splitting of flux vectors into subvectors by similarity transformations so that each subvector has associated with it a specified eigenvalue spectrum. As a consequence of flux vector splitting, new explicit and implicit dissipative finite-difference schemes are developed for first-order hyperbolic systems of equations. Appropriate one-sided spatial differences for each split flux vector are used throughout the computational field even if the flow is locally subsonic. The results of some preliminary numerical computations are included.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Computational Physics; 40; Apr. 198
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  • 86
    Publication Date: 2011-08-18
    Description: An analysis is made of the influence of landing gear deflection characteristics on aircraft performance on the ground up to rotation. A quasi-steady dynamic equilibrium state is assumed, including other simplifying assumptions such as calm air conditions and normal aircraft lift and drag. Ground incidence is defined as the angle made by the mean aerodynamic chord of the wing with respect to the ground plane, and equations are given for force and balance which determine the quasi-equilibrium conditions for the aircraft during ground roll. Results indicate that the landing gear deflections lead to a substantial increase in the angle of attack, and the variation in the ground incidence due to landing gear flexibility could be as much as + or - 50%, and the reduction in tail load requirements almost 25%.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Journal of Aircraft; 18; Nov. 198
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  • 87
    Publication Date: 2011-08-18
    Description: The design complexity and size of convectively-cooled engine and airframe structures for hypersonic transports necessitate the use of large general purpose computer programs for both thermal and structural analyses. Generally thermal analyses are based on the lumped-parameter finite difference technique, and structural analyses are based on the finite element technique. Differences in these techniques make it difficult to achieve an efficient interface. It appears, therefore, desirable to conduct an integrated analysis based on a common technique. A summary is provided of efforts by NASA concerned with the development of an integrated thermal structural analysis capability using the finite element method. Particular attention is given to the development of conduction/forced-convection finite element methodology and applications which illustrate the capabilities of the developed concepts.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
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  • 88
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    Publication Date: 2011-08-18
    Description: It is noted that several terms in the two-point spectral equation for homogeneous turbulence can be interpreted as spectral-transfer terms; that is, they represent the net rate of energy transfer into a wavenumber region from all other wavenumbers. This holds for terms associated with both turbulence and self-interaction and interaction between turbulence and mean gradients. It is not seen as obvious, however, that similar interpretations apply when the turbulence is not homogeneous. In particular, one might question the interpretation for the terms associated with turbulence self-interaction because the condition of homegeneity is generally used in making the interpretation. It is the purpose here to consider whether terms interpretable as transfer terms exist in the equations for inhomogeneous turbulence. It is found that certain terms in the two-point spectral equation can be interpreted as transfer terms.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Physics of Fluids; 24; Oct. 198
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  • 89
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    Publication Date: 2011-08-18
    Description: A solution to the rapid-distortion theory for small-scale turbulence in flow round an axisymmetric obstacle is derived. General formulae for velocity covariances and Eulerian time scales are obtained and are evaluated for the particular case of flow round a sphere. The large-scale limit for this flow is also discussed.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Quarterly Journal of Mechanics and Applied Mathematics; 34; Nov. 198
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  • 90
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    Publication Date: 2011-08-18
    Description: A correction is presented for a previously published inconsistency in predicted airframe noise values, which were based on approach velocities lower than those required for FAA certification. New figures are given for the following aircraft: DC-9-30, 727-200, A300-B2, L-1011, DC-10-10, and 747-200B. The new levels average 2.3 dB higher than those calculated for typical approach speeds.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Journal of Aircraft; 18; Sept
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  • 91
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    Publication Date: 2011-08-18
    Description: The considered study is based on new theoretical concepts regarding a post-instability model of a fluid discussed by Zak (1980). The model permits the completion of the governing equations of turbulence by introducing multivalued fields of velocities. Attention is given to the mechanism of energy dissipation, the characteristic wave propagation, a simplified model, the formation of turbulence around stagnation points, the formulation of boundary conditions, and the mechanism of turbulence formation. The mechanism of turbulence formation can be understood as propagation of initial discontinuities from the boundaries into a flow with the characteristic velocity which is defined by the normal (to the boundary) velocity components. These components emerge at the boundary as a result of jumps in the tangential components due to the continuity equation.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Mechanics Research Communications; 8; 2, 19; 1981
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  • 92
    facet.materialart.
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    Publication Date: 2011-08-18
    Description: Hot-wire measurements in an incompressible rectangular jet, issuing into a quiet environment at ambient conditions, are presented. A blow-down-type air supply system was used to provide the airflow to a cylindrical settling chamber 1.75 m in length and 0.6 m in diameter. The measurements were made with constant-temperature anemometers in conjunction with linearizers. The two signals from the linearizers were sent through a sum and difference unit which was calibrated from dc to 100 kHz. The distributions of mean velocity and the turbulence shear stresses were measured in the two central planes of the jet stations up to 115 widths downstream of the nozzle exit. Three distinct regions characterized the jet flow field: a potential core origin, a two-dimensional-type region, and an axisymmetric type region. The onset of the second region appeared to be at a location where the shear layers separated by the short dimension of the nozzle meet; and the third region occurred at a downstream location where the two shear layers from the short edges of the nozzle meet. In the central plane, similarity was found both in the mean velocity and shear stress profiles beyond 30 widths downstream of the nozzle exit; profiles of rms velocity showed similarity in the second, but not the third region.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: Journal of Fluid Mechanics; 107; June 198
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  • 93
    Publication Date: 2011-08-18
    Description: The development of a comprehensive analytical model of rotorcraft aerodynamics and dynamics is described. Particular emphasis is given to describing the reasons behind the choices and decisions involved in constructing the model. The analysis is designed to calculate rotor performance, loads and noise; helicopter vibration and gust response; flight dynamics and handling qualities; and system aeroelastic stability. It is intended for use in the design, testing and evaluation of a wide class of rotors and rotorcraft, and to be the basis for further development of rotary wing theories. The general characteristics of the geometric, structural, inertial, and aerodynamic models used for the rotorcraft components are described, including the assumptions introduced by the chosen models and the resulting capabilities and limitations. Finally, some examples from recent applications of the analysis are given.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Vertica; 5; 2, 19; 1981
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  • 94
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    Publication Date: 2011-08-18
    Description: The utility of the cryogenic high Reynolds number test facility as a production tunnel is evaluated. Aerodynamic performance evaluation, numerical wing design verification, and high Reynolds number theoretical extensions are considered. A priority ranking of NTF uses from an airframe development viewpoint is presented.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Langley Research Center High Reynolds Number Res. - 1980; p 149-152
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  • 95
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    Publication Date: 2011-08-18
    Description: Governing equations are developed for a simple capacitive heat exchanger. This type of heat exchanger consists of hot spherical particles falling through an ascending cold gas stream. The assumptions made in deriving the continuity, momentum and energy equations are clearly stated. The analysis yields a system of first order, ordinary, nonlinear equations which form a complex boundary value problem. The method of solution is presented together with a comparison between the performance of capacitive heat exchangers and conventional counter flow ones.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: The Telecommun. and Data Acquisition Progr. Rept. 42-64; p 207-221
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  • 96
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    Publication Date: 2011-08-18
    Description: The significant technology items of the Concorde and the conceptual MCD baseline advanced supersonic transport are compared. The four major improvements are in the areas of range performance, structures (materials), aerodynamics, and in community noise. Presentation charts show aerodynamic efficiency; the reoptimized wing; low scale lift/drag ratio; control systems; structural modeling and analysis; weight and cost comparisons for superplasticity diffusion bonded titanium sandwich structures and for aluminum brazed titanium honeycomb structures; operating cost reduction; suppressor nozzles; noise reduction and range; the bicone inlet; a market summary; environmental issues; high priority items; the titanium wing and fuselage test components; and technology validation.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2; p 873-888
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  • 97
    Publication Date: 2011-08-18
    Description: Graphite/epoxy panels with buffer strips were tested in tension to measure their residual strength with crack-like damage. Panels were made with 45/0/-45/90(2S) and 45/0/450(2S) layups. The buffer strips were parallel to the loading directions. They were made by replacing narrow strips of the 0 deg graphite plies with strips of either 0 deg S-Glass/epoxy or Kevlar-49/epoxy on either a one for one or a two for one basis. In a third case, O deg graphite/epoxy was used as the buffer material and thin, perforated Mylar strips were placed between the 0 deg piles and the cross-plies to weaken the interfaces and thus to isolate the 0 deg plies. Some panels were made with buffer strips of different widths and spacings. The buffer strips arrested the cracks and increased the residual strengths significantly over those plain laminates without buffer strips. A shear-lag type stress analysis correctly predicted the effects of layups, buffer material, buffer strip width and spacing, and the number of plies of buffer material.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Supersonic Cruise Res., 1979, Pt. 2; p 657-673
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  • 98
    Publication Date: 2011-08-18
    Description: NASA Langley Research Center SCAR in-house structural studies are reviewed. In methods development, advances include a new system of integrated computer programs called ISSYS, progress in determining aerodynamic loads and aerodynamically induced structural loads (including those due to gusts), flutter optimization for composite and metal airframe configurations using refined and simplified mathematical models, and synthesis of active controls. Results given address several aspects of various SCR configurations. These results include flutter penalties on composite wing, flutter suppression using active controls, roll control effectiveness, wing tip ground clearance, tail size effect on flutter, engine weight and mass distribution influence on flutter, and strength and flutter optimization of new configurations. The ISSYS system of integrated programs performed well in all the applications illustrated by the results, the diversity of which attests to ISSYS' versatility.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Supersonic Cruise Res., 1979, Pt. 2; p 617-656
    Format: text
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  • 99
    Publication Date: 2011-08-18
    Description: The superplastically formed diffusion-bonded (SPF/DB) program has developed successfully and far enough to recommend that a major structural program to validate the weight and cost of SPF/DB sandwich titanium structure should be initiated. The NASA Langley study of wing and fuselage SPF/DB sandwich panels shows that this process is potentially structurally efficient. The Douglas SPF/DB expanded sandwich process that utilizes a welded core sheet that expands to face sheets proves to be very efficient. The theoretical weight optimization design charts for the wing and fuselage concepts were validated by small-scale tests. Mnay design applications were fabricated. Projecting the results of an SPF/DB sandwich airframe structure to a MDC AST design shows significant weight and cost savings. A 6 percent lower direct operating cost was calculated. A growth AST utilizing composites, metal matrices, and SPF/DB sandwich shows future promise for a post-1990 technology readiness. Titanium SPF/DB sandwich, compared to presently available aluminum structure, is superior for application to a Mach 2.2 supersonic transport.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA. Langley Research Center Supersonic Cruise Res., 1979, Pt. 2; p 589-616
    Format: text
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  • 100
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    Unknown
    In:  Other Sources
    Publication Date: 2011-08-18
    Description: A definition for the large-scale coherent structure is presented, and the nature and role of coherent structures in turbulent shear flows are examined. The equations governing the coherent motions and the experimental considerations as well as constraints in the investigations of coherent structures in wall-bounded and free turbulent shear flows are discussed. Results from a few of our recent and on-going studies of coherent structures in excited and unexcited free turbulent shear flows are reviewed. These results show that coherent structures are dominant in transport in the early stages of their formation, but not in the self-preserving regions of turbulent shear flows.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: vol. 4; Aug. 198
    Format: text
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