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  • Other Sources  (2,751)
  • STRUCTURAL MECHANICS  (1,991)
  • Seismology
  • Industrial Chemistry
  • Inorganic Chemistry
  • 1990-1994  (2,686)
  • 1950-1954  (50)
  • 1920-1924
Collection
Years
Year
  • 1
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    In:  Geophys. J. Int., Warszawa, Elsevier, vol. 118, no. 1-2, pp. 693-706, pp. 1960, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Location ; Seismology ; Hypocentral depth ; Data analysis / ~ processing ; GJI
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  • 2
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    In:  Terra Nova, Potsdam, ZIPE, vol. 6, no. 6979, pp. 291-300, pp. 2501, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Seismology ; Earthquake ; Tectonics
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  • 3
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    In:  Geologie en Mijnbouw, Potsdam, ZIPE, vol. 73, no. 6979, pp. 181-197, pp. 2501, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Earthquake ; Source parameters ; Magnitude ; Seismology ; Fault plane solution, focal mechanism ; Location ; Tectonics
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  • 4
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    In:  Phys. Earth Plan. Int., Warszawa, Army Corps of Engineers, Woodward-Clyde Consultants, vol. 85, no. 1-3, pp. 293-318, pp. B05310, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Seismology ; Source ; SH waves ; Earthquake ; Inversion ; PEPI
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  • 5
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    In:  Phys. Earth Plan. Int., Bonn, Pergamon, vol. 82, no. 4, pp. 271-276, pp. 2018, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1994
    Keywords: Quality factor ; FractureT ; Attenuation ; Seismology ; PEPI
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  • 6
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    In:  Eos, Trans., Am. Geophys. Un., Berlin, Schweizerbart'sche Verlagsbuchhandlung, vol. 75, no. 48, pp. 563, pp. L07302, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: CMB ; Geothermics ; earth Core ; Seismology
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  • 7
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    In:  J. Geophys. Res., London, Icelandic Meteorological Office, Ministry for the Environment University of Iceland, vol. 99, no. 1, pp. 11859-11877, pp. TC1011, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: Volcanology ; Non-linear effects ; Fluids ; Dynamic ; Seismology ; JGR
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  • 8
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    In:  Geophys. J. Int., London, Icelandic Meteorological Office, Ministry for the Environment University of Iceland, vol. 117, no. 4, pp. 345-364, pp. B02206, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: Stress ; Seismicity ; Modelling ; Seismology ; GJI
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  • 9
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    In:  Ann. Rev. Earth Planet. Sci., Amsterdam, Elsevier Scientific Publishing Company, vol. 22, no. 50, pp. 207-237, pp. 2265, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: Review article ; Seismology ; Source ; ANREV
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  • 10
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    In:  Geophys. Res. Lett., Luxembourg, Conseil de l'Europe, vol. 21, no. 1, pp. 9-12, pp. L24312, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Moment tensor ; Fault plane solution, focal mechanism ; Seismology ; Wave form analysis ; Inversion ; GRL ; 7215 ; Seismology ; Earthquake ; parameters ; 7255 ; Surface ; waves ; and ; free ; oscillations ; nokms
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  • 11
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    In:  Geophys. Res. Lett., Basel, Elsevier Science Publishers, vol. 21(14), no. B3, pp. 1491-1494, pp. B03304, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; China ; GRL
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  • 12
    Publication Date: 1994
    Keywords: Seismology ; Volcanology ; Location ; Fluids
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  • 13
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    In:  Bull. Seism. Soc. Am., Chengdu, Sichuan, China, 4, vol. 84(2), no. B3, pp. 307-323, pp. 1334, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; BSSA
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  • 14
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    In:  J. Geophys. Res., New York, 1-2, vol. 99, no. 19, pp. 2591-2600, pp. 2554, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Waves ; Wave propagation ; Non-linear effects ; Seismology ; JGR
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  • 15
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    In:  J. Geophys. Res., New York, August, vol. 99/B7, no. 3, pp. 13655-13665, pp. B05S05, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; China ; Seismology ; earth mantle ; JGR
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  • 16
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    In:  Tectonophys., Kalamazoo, Michigan 49001, The Upjohn Company, vol. 233, no. 4, pp. 253-264, pp. L09603, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Location ; Seismology
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  • 17
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    In:  Seismological Res. Lett., L'wiw, Inst. f. Theoret. Geodäsie, vol. 65 (1), no. 4, pp. 20, pp. B01408, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; Conference abstr. ; SRL
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  • 18
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    In:  Phys. Earth Plan. Int., Luxembourg, Conseil de l'Europe, vol. 83, no. 5, pp. 41-56, pp. L20305, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Source parameters ; Low frequency ... ; Data analysis / ~ processing ; PEPI
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  • 19
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    In:  Geophys. J. Int., Stuttgart, Schweizerbart'sche Verlagsbuchhandlung, vol. 118, no. 11/12, pp. 802-807, pp. L08309, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: Inhomogeneity ; Seismology ; Travel time ; Vertical seismic profiling ; Borehole geophys. ; GJI
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  • 20
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    In:  Geophys. J. Int., Amsterdam, Schweizerbart'sche Verlagsbuchhandlung, vol. 117, no. 44, pp. 591-609, pp. L12S09, (ISSN 0016-8548, ISBN 3-510-50045-8)
    Publication Date: 1994
    Keywords: Seismology ; RMS ; Lg-waves ; Nuclear explosion ; GJI
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  • 21
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    In:  J. Geophys. Res., Chengdu, Sichuan, China, 4, vol. 99, no. B3, pp. 11705-11722, pp. 1334, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Fault zone ; Seismology ; Waves ; Channel waves ; Earthquake ; JGR
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  • 22
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    In:  Geophys. J. Int., Hannover, Conseil de l'Europe, vol. 119, no. 1, pp. 783-790, pp. L24314, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Anisotropy ; Seismology ; Stefansson ; GJI
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  • 23
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    In:  Eos, Trans., Am. Geophys. Un., Paris, Conseil de l'Europe, vol. 75, no. 13, pp. 150f., 154, pp. L01306, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Project report/description ; OBS ; Seismology
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  • 24
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    In:  Tectonophys., Washington, D.C., American Geophysical Union, vol. 231, no. 3, pp. 311-323, pp. L08304, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Fault plane solution, focal mechanism ; Seismology ; Earthquake catalog
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  • 25
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    In:  DGG Mittlg., L'wiw, 3-4, vol. 211, no. 4, pp. 53-54, pp. L24312, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Proceedings of a conference ; Geodesy ; Gravimetry, Gravitation ; Seismology ; Earthquake precursor: prediction research ; Kumpel
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  • 26
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    In:  J. Geophys. Res., Luxembourg, Conseil de l'Europe, vol. 99, no. 1, pp. 15457-15467, pp. L24312, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Moment tensor ; Seismology ; Source mechanics ; JGR
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  • 27
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    In:  GSA Today, Tulsa, 450 pp.; 2nd modified and expanded ed., Society of Exploration Geophysics, vol. 4, no. 5, pp. 129, 132-134, pp. B12408, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Real time earthquake monitoring ; Seismology ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Fracture
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  • 28
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    In:  Rev. Geophys., Paris, Conseil de l'Europe, vol. 32, no. 1-2, pp. 115-137, pp. L01306, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; ConvolutionE ; GeodesyY ; Tomography ; Review article
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  • 29
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    In:  Bull. Seism. Soc. Am., vol. 84, no. 3-4, pp. 724-734
    Publication Date: 1994
    Keywords: Local earthquakes ; Source ; Seismology ; Earthquake ; Source parameters ; multiple ; ruptures ; BSSA
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  • 30
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    In:  Geologie en Mijnbouw, Bonn, Inst. f. Theoret. Geodäsie, vol. 73, no. 2, pp. 199-214
    Publication Date: 1994
    Keywords: Fault plane solution, focal mechanism ; Source parameters ; Earthquake ; Aftershocks ; Seismology
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  • 31
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    In:  Geophys. J. Int., Luxembourg, Conseil de l'Europe, vol. 119, no. 2, pp. 574-594, pp. 1892
    Publication Date: 1994
    Keywords: Velocity depth profile ; Teleseismic events ; Seismology ; GJI
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  • 32
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    In:  Eos, Trans., Am. Geophys. Un., San Francisco, Pergamon, vol. 75, no. 20, pp. 225, pp. 1246
    Publication Date: 1994
    Keywords: SEDI ; Seismic networks ; Seismology
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  • 33
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    In:  Geophys. J. Int., Warszawa, Elsevier, vol. 118, no. 1-2, pp. 680-692, pp. 1960, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Location ; Seismology ; Data analysis / ~ processing ; GJI
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  • 34
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    In:  Geophys. J. Int., Leipzig, 3-4, vol. 116, no. 1, pp. 663-672, pp. L19606, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Source parameters ; Seismology ; Earthquake ; Inversion ; Surface waves ; GJI
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  • 35
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    In:  Earth planet. Sci. Lett., Potsdam, ZIPE, vol. 121, no. 4, pp. 385-403, pp. 2156, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Geothermics ; earth mantle ; Tomography ; Seismology ; Mineralogy ; Modelling ; Cadek
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  • 36
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    In:  DGG Mittlg., Warszawa, Conseil de l'Europe, vol. 5, no. 1-2, pp. 10-19, pp. 1095, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Project report/description ; Stress ; Geothermics ; Seismology ; Laboratory measurements ; Cermak
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  • 37
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    In:  Annali di Geofisica, Roma, Publicazioni dell'Istituto Nazionale di Geofisica, vol. 37, no. 3, pp. V, pp. B09304, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Proceedings of a conference ; Nuclear explosion ; Seismology ; Data analysis / ~ processing ; Detectors ; Discrimination ; Magnitude ; Location
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  • 38
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    In:  J. Volc. Geoth. Res., Roma, Publicazioni dell'Istituto Nazionale di Geofisica, vol. 62, no. 2, pp. 467-496, pp. B04102, (ISBN: 0-12-018847-3)
    Publication Date: 1994
    Keywords: Earthquake precursor: prediction research ; Volcanology ; Seismology ; Earthquake precursor: statistical anal. of seismicity
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  • 39
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    In:  Geologie en Mijnbouw, Stockholm, Wissenschaftliche Buchgesellschaft, vol. 4, no. E53, pp. 1-4, pp. L11308, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Stress ; Fault plane solution, focal mechanism ; Seismology ; rifting ; Conference abstr.
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  • 40
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    In:  Tectonophys., Oslo, Wiley, vol. 237, no. 35, pp. 73-86, pp. B08303, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Fault plane solution, focal mechanism ; Seismology ; Rognvaldsson
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  • 41
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    In:  Phys. Earth Plan. Int., Oslo, Wiley, vol. 84, no. 23, pp. 179-192, pp. L02304, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Inelastic ; Low frequency ... ; Surface waves ; Attenuation ; PEPI
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  • 42
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    In:  Science, Basel, Inst. f. Geophys., Ruhr-Univ. Bochum, vol. 263, no. 1-2, pp. 1105-1111, pp. 1019, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Plate tectonics ; ConvolutionE ; Anisotropy ; Seismology ; earth mantle
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  • 43
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    In:  Geophys. J. Int., Hokkaido University, Inst. f. Geophys., Ruhr-Univ. Bochum, vol. 117, no. 1-4, pp. 487-494, pp. 8038, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Scattering ; Seismology ; ConvolutionR ; Body waves ; Coda (waves, ~ of seismograms) ; GJI
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  • 44
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    In:  J. Volc. Geoth. Res., Hokkaido University, Inst. f. Geophys., Ruhr-Univ. Bochum, vol. 63, no. 105, pp. 111-128, pp. 2339, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Volcanology ; Seismology ; Seismicity
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  • 45
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    In:  Natural Hazards, Stuttgart, Ferdinand Enke Verlag, vol. 10, no. 2, pp. 275-296, pp. L07611, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Site amplification ; Earthquake engineering, engineering seismology ; Seismology ; Modelling ; Statistical investigations ; NATHAZ ; SRICHWALSKI
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  • 46
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    In:  Geophysical Journal International, Stuttgart, Ferdinand Enke Verlag, vol. 119, no. 2, pp. 31-43, pp. L07611, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Earthquake ; Modelling ; Statistical investigations ; High frequency ... ; Strong motions ; Seismology ; GJI
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  • 47
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    In:  Phys. Earth Plan. Int., Luxembourg, Deutsche Geophys. Gesellschaft, vol. 85, no. B11, pp. 265-272, pp. B11307, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Stress drop ; Seismology ; PEPI
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  • 48
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    In:  Eos, Trans., Am. Geophys. Un., Luxembourg, Inst. Electrical & Electronics Engineers, vol. 75, no. 39, pp. 449, pp. B06303, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Surface waves ; Review article
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  • 49
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    In:  J. Volc. Geoth. Res., Würzburg, Pergamon, vol. 62, no. 49, pp. 153-182, pp. B05S01, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Volcanology
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  • 50
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    In:  Eos, Trans., Am. Geophys. Un., Berlin, Pergamon, vol. 75, no. 10, pp. 117, pp. B04306, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Attenuation
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  • 51
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    In:  Geophys. Res. Letters, Veldhoven, Kluwer, vol. 21, no. 6, pp. 457-460, pp. 2141, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; earth mantle ; Seismology ; Seismic networks ; GRL
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  • 52
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    In:  Eos, Trans., Am. Geophys. Un., Leipzig, Akad. Nauk SSSR, vol. 75, no. 28, pp. 313, pp. B01308, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Nuclear explosion ; CTBT ; Seismology ; Detectors
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  • 53
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    In:  Bull. Seism. Res., Kunming, China, D. Reidel Publishing Company, vol. 17, no. B11, pp. 30-39, pp. L09303, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Seismicity ; Earthquake precursor: statistical anal. of seismicity
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  • 54
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    American Geophysical Union
    In:  London, American Geophysical Union, vol. 1, no. 3, pp. 632 pp., (ISBN-10: 1-84628-053-2, ISBN-13:978-1-84628-053-5, eISBN 1-84628-054-0, xx + 591 pp. + CD-ROM)
    Publication Date: 1994
    Keywords: Seismology ; GeodesyY ; Synthetic seismograms
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  • 55
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    In:  Bull. Seism. Soc. Am., Washington D.C., Bundesanstalt für Geowissenschaften und Rohstoffe, vol. 84, no. 2, pp. 359-365, pp. L09611
    Publication Date: 1994
    Description: A prototype early warning system to provide San Francisco and Oakland, California a few tens-of-seconds warning of incoming strong ground shaking from already-occurred M = or 〉 3.7 aftershocks of the magnitude 7.1 17 October 1989 Loma Prieta earthquake was operational on 28 October 1989. The prototype system consisted of ground motion sensors in the epicentral area, a central receiver, a radio repeater, and radio receivers. One of the radio receivers provided about 20 sec of warning before shaking from the M 4.5 Loma Prieta aftershock that occurred on 2 November 1989 at 0550 UTC. In its first 6 months of operation, the system generated triggers for all 12 M 〉 3.7 aftershocks for which trigger documentation is preserved. Because the prototype system demonstrated that potentially useful warnings of strong shaking from aftershocks are feasible, the USGS has completed a portable early warning system for aftershocks that can be deployed anywhere. One of the radio receivers was deployed at the California Department of Transportation (CALTransformations) headquarters at the damaged Cypress Street section of the I-880 freeway in Oakland, California on 28 October 1989 and provided about 20 sec ..., did not trigger on any M〈or=3.6 aftershocks, and produced one false trigger as a result of a now-corrected single point of failure design flaw.
    Keywords: Seismology ; Early warning systems (earthquakes, volcanic eruptions, tsunamis etc.) ; Aftershocks ; Detectors ; Location ; Magnitude ; Instruments ; Source parameters ; Strong motions ; Seismometer ; BSSA ; San ; Francisco ; Oakland ; California ; Loma ; Prieta ; ground ; motion ; sensors ; epicentral ; area ; central ; receiver ; radio ; repeater ; radio ; receivers ; California ; Department ; of ; Transportation ; headquarters ; CALTransformations ; I-880 ; freeway ; triggers ; prototype ; system ; USA
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  • 56
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    In:  J. Volc. Geoth. Res., Luxembourg, Am. Soc. Mech. Eng., vol. 61, no. 8, pp. 239-251, pp. L12311, (ISBN 0-471-26610-8)
    Publication Date: 1994
    Keywords: Seismicity ; Volcanology ; Seismology ; Waves
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  • 57
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    In:  Pageoph, Luxembourg, Am. Soc. Mech. Eng., vol. 143, no. 1-2, pp. 513-536, pp. 2099, (ISBN 0-471-26610-8)
    Publication Date: 1994
    Keywords: Wave propagation ; Synthetic seismograms ; Modelling ; Site amplification ; Seismology ; Fah ; Faeh
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  • 58
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    In:  Bull. Seism. Soc. Am., Luxembourg, Am. Soc. Mech. Eng., vol. 84, no. 1-2, pp. 383-399, pp. 2099, (ISBN 0-471-26610-8)
    Publication Date: 1994
    Keywords: Seismology ; Strong motions ; Site amplification ; Modelling ; Synthetic seismograms ; combination ; BSSA ; Fah ; Faeh ; Zahradnik
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  • 59
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    In:  Bull. Seism. Soc. Am., Heidelberg, 1, vol. 84, no. 4-5, pp. 646-659, pp. B01401, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1994
    Keywords: Source ; Seismology ; Earthquake ; Global Positioning System ; southern ; California ; BSSA
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  • 60
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    In:  Science, Klagenfurt, Nuclear Technology Publ., vol. 264, no. 2, pp. 804-809, pp. L14312, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1994
    Keywords: Seismology ; Source ; Fault plane solution, focal mechanism ; CLVD ; nokms
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  • 61
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    In:  J. Geophys. Res., Bonn, Pergamon, vol. 99, no. 4, pp. 11723-11730, pp. 2018, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1994
    Keywords: Nuclear explosion ; DeconvolutionP ; Magnitude ; Energy (of earthquakes) ; Source ; Seismology ; Detectors ; JGR
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  • 62
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    In:  J. Geophys. Res., Luxembourg, Am. Soc. Mech. Eng., vol. 99, no. 6, pp. 11643-11662, pp. L12311, (ISBN 0-471-26610-8)
    Publication Date: 1994
    Keywords: Body waves ; Surface waves ; Earthquake precursor: prediction research ; Earthquake precursor: statistical anal. of seismicity ; Seismology ; Waves ; JGR ; Earthquake
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  • 63
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    In:  Earth planet. Sci. Lett., Kleinmachnow, Dt. Geophys. Ges. e. V., vol. 122, no. 6, pp. 89-101, pp. B05401, (ISBN: 0534351875, 2nd edition)
    Publication Date: 1994
    Keywords: Seismology ; Earth model, also for more shallow analyses ! ; Subduction zone ; phase ; transition
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  • 64
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    In:  Geophys. J. Int., Kyoto, AGU, vol. 116, no. 1, pp. 673-682, pp. L07305, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Source parameters ; Seismology ; Earthquake ; Spectrum ; Body waves ; Seismic networks ; GJI
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  • 65
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    In:  Bull. Seism. Soc. Am., Basle, Wiley, vol. 84, no. 1, pp. 1169-1183, pp. 1264, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Three dimensional ; Scattering ; Seismology ; Two-dimensional ; BSSA ; Sanchez
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  • 66
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    In:  Geophys. Res. Lett., Luxembourg, Conseil de l'Europe, vol. 21(14), no. 28, pp. 1507-1510, pp. 2131, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Review article ; plume ; Seismology ; earth mantle ; Volcanology ; ConvolutionE ; GRL
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  • 67
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    In:  Phys. Earth Plan. Int., Minsk, Polish Geothermal Association, vol. 82, no. 7, pp. 1-7, pp. L24309, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Seismicity ; Moment tensor ; Filter- ; PEPI
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  • 68
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    In:  Geophys. J. Int., Dordrecht, National Academy of Sciences of the USA, vol. 119, no. 5-6, pp. 949-963, pp. TC5003, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; Shear waves ; GJI
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  • 69
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    In:  J. Geophys. Int., Stockholm, Wissenschaftliche Buchgesellschaft, vol. 119, no. E53, pp. 402-420, pp. L11308, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; earth mantle ; rifting
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  • 70
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    In:  Geophys. J. Int., Luxembourg, National Academy of Sciences of the USA, vol. 119, no. 2, pp. 260-268, pp. B05311, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Earthquake ; Source ; Aftershocks ; GJI
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  • 71
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    In:  Phys. Earth Plan. Int., Luxembourg, Lawrence Livermore National Laboratory, vol. 86, no. 1-2, pp. 5-24, pp. B05311, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; GeodesyY ; GeodesyY ; PEPI
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  • 72
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    In:  Bull. Seism. Res., Washington, D.C., AGU, vol. 17, no. 1-4, pp. 46-55, pp. B05204, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: China ; Earthquake ; Seismology ; Crustal deformation (cf. Earthquake precursor: deformation or strain)
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  • 73
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    In:  Geophys. J. Int., Taipei, AGU, vol. 118, no. 6, pp. 57-74, pp. B05403, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Travel time ; Amplitude ; Seismology ; Seismic arrays ; GJI
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  • 74
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    In:  J. Phys. Earth, Reykjavík, Icelandic Meteorological Office, Ministry for the Environment, University of Iceland, vol. 42, no. 5694, pp. 425-437, pp. 2212, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Fracture ; Elasticity ; Seismology ; Elasticity theory of dislocations ; JPE
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  • 75
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    In:  Eos, Trans., Am. Geophys. Un., Hannover, Polish Geothermal Association, vol. 75, no. 22, pp. 249, pp. 1051, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Earthquake precursor: prediction research ; Review article ; ENDNOTE?
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  • 76
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    In:  Geophys. J. Int., Washington, D.C., AGU, vol. 118, no. 11, pp. 20-30, pp. 1047, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Source ; Seismology ; Fault plane solution, focal mechanism ; Moment tensor ; GJI
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  • 77
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    In:  Eos, Trans., Am. Geophys. Un., Leyden, Noordhoff International Publishing, vol. 75, no. 24, pp. 265, pp. B04306, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Nuclear explosion ; CTBT ; Seismology ; Detectors
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  • 78
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    In:  Bull. Seism. Soc. Am., Hannover, D. Reidel Publishing Company, vol. 84, no. 4, pp. 974-1002, pp. L09303, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; scaling ; Source parameters ; Magnitude ; BSSA
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  • 79
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    In:  Bull. Seism. Soc. Am., Kunming, China, 3-4, vol. 84, no. 3, pp. 91-104, pp. B05301, (ISSN: 1340-4202)
    Publication Date: 1994
    Keywords: Seismology ; Source parameters ; Location ; Broad-band ; Inversion ; BSSA
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  • 80
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    Blackwell Scientific Publications
    In:  736 pp., Blackwell Scientific Publications, vol. 5, no. XVI:, pp. 227-235, (ISBN 0632036990)
    Publication Date: 1994
    Keywords: Handbook of geophysics ; Handbook of geology ; Seismics (controlled source seismology) ; Plate tectonics ; Seismology ; Gravimetry, Gravitation
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  • 81
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    Inst. f. Meteorol. und Geophys., Univ. Frankfurt am Main, 124 pp.
    In:  Diploma Thesis, Calgary, Inst. f. Meteorol. und Geophys., Univ. Frankfurt am Main, 124 pp., vol. C 560, 183 pp., no. 78-694, pp. 1-113, (ISBN 3-933346-037)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; Seismic networks
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  • 82
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    In:  Eos, Trans., Am. Geophys. Un., Luxembourg, Conseil de l'Europe, vol. 75, no. 28, pp. 313, pp. 1484, (ISSN 0343-5164)
    Publication Date: 1994
    Keywords: Volcanology ; Seismology ; Bruestle ; Brustle
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  • 83
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    In:  Geophys. J. Int., Luxembourg, Conseil de l'Europe, vol. 119, no. 6, pp. 561-573, pp. 1484, (ISSN 0343-5164)
    Publication Date: 1994
    Keywords: AnisotropyS ; Seismology ; Shear waves ; GJI
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  • 84
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    In:  Other Sources
    Publication Date: 2011-08-24
    Description: The analysis of balloon envelopes by the finite element (FE) method is plagued by convergence problems. A pratical FE analysis approach is based on the fact that in thin shells with non-zero Gaussian curvature the membrane solution component is essentially decoupled from the bending solution component. A proxy-problem is solved by using a small artificial bending stiffness that assures convergence without significantly affecting the membrane solution component. This approach has been previously validated on slightly overpressurized balloon envelopes. Extensions of this approach to more difficult problems in the structural analysis of balloon envelopes are presented. The convergence forcing modelling measures are discussed. Implications of the findings of the analysis results to future balloon designs are also discussed.
    Keywords: STRUCTURAL MECHANICS
    Type: Advances in Space Research (ISSN 0273-1177); 14; 2; p. (2)43-(2)47
    Format: text
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  • 85
    Publication Date: 2011-08-24
    Description: The Composite Plate Buckling Analysis Program (COMPPAP) was written to help engineers determine buckling loads of orthotropic (or isotropic) irregularly shaped plates without requiring hand calculations from design curves or extensive finite element modeling. COMPPAP is a one element finite element program that utilizes high-order displacement functions. The high order of the displacement functions enables the user to produce results more accurate than traditional h-finite elements. This program uses these high-order displacement functions to perform a plane stress analysis of a general plate followed by a buckling calculation based on the stresses found in the plane stress solution. The current version assumes a flat plate (constant thickness) subject to a constant edge load (normal or shear) on one or more edges. COMPPAP uses the power method to find the eigenvalues of the buckling problem. The power method provides an efficient solution when only one eigenvalue is desired. Once the eigenvalue is found, the eigenvector, which corresponds to the plate buckling mode shape, results as a by-product. A positive feature of the power method is that the dominant eigenvalue is the first found, which is this case is the plate buckling load. The reported eigenvalue expresses a load factor to induce plate buckling. COMPPAP is written in ANSI FORTRAN 77. Two machine versions are available from COSMIC: a PC version (MSC-22428), which is for IBM PC 386 series and higher computers and compatibles running MS-DOS; and a UNIX version (MSC-22286). The distribution medium for both machine versions includes source code for both single and double precision versions of COMPPAP. The PC version includes source code which has been optimized for implementation within DOS memory constraints as well as sample executables for both the single and double precision versions of COMPPAP. The double precision versions of COMPPAP have been successfully implemented on an IBM PC 386 compatible running MS-DOS, a Sun4 series computer running SunOS, an HP-9000 series computer running HP-UX, and a CRAY X-MP series computer running UNICOS. COMPPAP requires 1Mb of RAM and the BLAS and LINPACK math libraries, which are included on the distribution medium. The COMPPAP documentation provides instructions for using the commercial post-processing package PATRAN for graphical interpretation of COMPPAP output. The UNIX version includes two electronic versions of the documentation: one in LaTex format and one in PostScript format. The standard distribution medium for the PC version (MSC-22428) is a 5.25 inch 1.2Mb MS-DOS format diskette. The standard distribution medium for the UNIX version (MSC-22286) is a .25 inch streaming magnetic tape cartridge (Sun QIC-24) in UNIX tar format. For the UNIX version, alternate distribution media and formats are available upon request. COMPPAP was developed in 1992.
    Keywords: STRUCTURAL MECHANICS
    Type: MSC-22428
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  • 86
    Publication Date: 2011-08-24
    Description: The Composite Plate Buckling Analysis Program (COMPPAP) was written to help engineers determine buckling loads of orthotropic (or isotropic) irregularly shaped plates without requiring hand calculations from design curves or extensive finite element modeling. COMPPAP is a one element finite element program that utilizes high-order displacement functions. The high order of the displacement functions enables the user to produce results more accurate than traditional h-finite elements. This program uses these high-order displacement functions to perform a plane stress analysis of a general plate followed by a buckling calculation based on the stresses found in the plane stress solution. The current version assumes a flat plate (constant thickness) subject to a constant edge load (normal or shear) on one or more edges. COMPPAP uses the power method to find the eigenvalues of the buckling problem. The power method provides an efficient solution when only one eigenvalue is desired. Once the eigenvalue is found, the eigenvector, which corresponds to the plate buckling mode shape, results as a by-product. A positive feature of the power method is that the dominant eigenvalue is the first found, which is this case is the plate buckling load. The reported eigenvalue expresses a load factor to induce plate buckling. COMPPAP is written in ANSI FORTRAN 77. Two machine versions are available from COSMIC: a PC version (MSC-22428), which is for IBM PC 386 series and higher computers and compatibles running MS-DOS; and a UNIX version (MSC-22286). The distribution medium for both machine versions includes source code for both single and double precision versions of COMPPAP. The PC version includes source code which has been optimized for implementation within DOS memory constraints as well as sample executables for both the single and double precision versions of COMPPAP. The double precision versions of COMPPAP have been successfully implemented on an IBM PC 386 compatible running MS-DOS, a Sun4 series computer running SunOS, an HP-9000 series computer running HP-UX, and a CRAY X-MP series computer running UNICOS. COMPPAP requires 1Mb of RAM and the BLAS and LINPACK math libraries, which are included on the distribution medium. The COMPPAP documentation provides instructions for using the commercial post-processing package PATRAN for graphical interpretation of COMPPAP output. The UNIX version includes two electronic versions of the documentation: one in LaTex format and one in PostScript format. The standard distribution medium for the PC version (MSC-22428) is a 5.25 inch 1.2Mb MS-DOS format diskette. The standard distribution medium for the UNIX version (MSC-22286) is a .25 inch streaming magnetic tape cartridge (Sun QIC-24) in UNIX tar format. For the UNIX version, alternate distribution media and formats are available upon request. COMPPAP was developed in 1992.
    Keywords: STRUCTURAL MECHANICS
    Type: MSC-22286
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  • 87
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    In:  Other Sources
    Publication Date: 2011-08-24
    Description: Structural flaws and cracks may grow under fatigue inducing loads and, upon reaching a critical size, cause structural failure to occur. The growth of these flaws and cracks may occur at load levels well below the ultimate load bearing capability of the structure. The Fatigue Crack Growth Computer Program, NASA/FLAGRO, was developed as an aid in predicting the growth of pre-existing flaws and cracks in structural components of space systems. The earlier version of the program, FLAGRO4, was the primary analysis tool used by Rockwell International and the Shuttle subcontractors for fracture control analysis on the Space Shuttle. NASA/FLAGRO is an enhanced version of the program and incorporates state-of-the-art improvements in both fracture mechanics and computer technology. NASA/FLAGRO provides the fracture mechanics analyst with a computerized method of evaluating the "safe crack growth life" capabilities of structural components. NASA/FLAGRO could also be used to evaluate the damage tolerance aspects of a given structural design. The propagation of an existing crack is governed by the stress field in the vicinity of the crack tip. The stress intensity factor is defined in terms of the relationship between the stress field magnitude and the crack size. The propagation of the crack becomes catastrophic when the local stress intensity factor reaches the fracture toughness of the material. NASA/FLAGRO predicts crack growth using a two-dimensional model which predicts growth independently in two directions based on the calculation of stress intensity factors. The analyst can choose to use either a crack growth rate equation or a nonlinear interpolation routine based on tabular data. The growth rate equation is a modified Forman equation which can be converted to a Paris or Walker equation by substituting different values into the exponent. This equation provides accuracy and versatility and can be fit to data using standard least squares methods. Stress-intensity factor numerical values can be computed for making comparisons or checks of solutions. NASA/FLAGRO can check for failure of a part-through crack in the mode of a through crack when net ligament yielding occurs. NASA/FLAGRO has a number of special subroutines and files which provide enhanced capabilities and easy entry of data. These include crack case solutions, cyclic load spectrums, nondestructive examination initial flaw sizes, table interpolation, and material properties. The materials properties files are divided into two types, a user defined file and a fixed file. Data is entered and stored in the user defined file during program execution, while the fixed file contains already coded-in property value data for many different materials. Prompted input from CRT terminals consists of initial crack definition (which can be defined automatically), rate solution type, flaw type and geometry, material properties (if they are not in the built-in tables of material data), load spectrum data (if not included in the loads spectrum file), and design limit stress levels. NASA/FLAGRO output includes an echo of the input with any error or warning messages, the final crack size, whether or not critical crack size has been reached for the specified stress level, and a life history profile of the crack propagation. NASA/FLAGRO is modularly designed to facilitate revisions and operation on minicomputers. The program was implemented on a DEC VAX 11/780 with the VMS operating system. NASA/FLAGRO is written in FORTRAN77 and has a memory requirement of 1.4 MB. The program was developed in 1986.
    Keywords: STRUCTURAL MECHANICS
    Type: MSC-21669
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  • 88
    Publication Date: 2011-08-24
    Description: Delaminations near the outer surface of a laminate are susceptible to local buckling and buckling-induced delamination propagation when the laminate is subjected to transverse impact loading. This results in a loss of stiffness and strength. TRBUCKL is an unique dynamic delamination buckling and delamination propagation analysis capability that can be incorporated into the structural analysis program, NASTRAN. This capability will aid engineers in the design of structures incorporating composite laminates. The capability consists of: (1) a modification of the direct time integration solution sequence which provides a new analysis algorithm that can be used to predict delamination buckling in a laminate subjected to dynamic loading; and (2) a new method of modeling the composite laminate using plate bending elements and multipoint constraints. The capability now exists to predict the time at which the onset of dynamic delamination buckling occurs, the dynamic buckling mode shape, and the dynamic delamination strain energy release rate. A procedure file for NASTRAN, TRBUCKL predicts both impact induced buckling in composite laminates with initial delaminations and the strain energy release rate due to extension of the delamination. In addition, the file is useful in calculating the dynamic delamination strain energy release rate for a composite laminate under impact loading. This procedure simplifies the simulation of progressive crack extension. TRBUCKL has been incorporated into COSMIC NASTRAN. TRBUCKL is a DMAP Alter for NASTRAN. It is intended for use only with the COSMIC NASTRAN Direct Transient Analysis (RF 9) solution sequence. The program is available as a listing only. TRBUCKL was developed in 1987.
    Keywords: STRUCTURAL MECHANICS
    Type: LEW-15323
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  • 89
    Publication Date: 2011-08-24
    Description: Predictions of fatigue crack growth behavior can be made with the Fatigue Crack Growth Structural Analysis (FASTRAN II) computer program. As cyclic loads are applied to a selected crack configuration with an initial crack size, FASTRAN II predicts crack growth as a function of cyclic load history until either a desired crack size is reached or failure occurs. FASTRAN II is based on plasticity-induced crack-closure behavior of cracks in metallic materials and accounts for load-interaction effects, such as retardation and acceleration, under variable-amplitude loading. The closure model is based on the Dugdale model with modifications to allow plastically deformed material to be left along the crack surfaces as the crack grows. Plane stress and plane strain conditions, as well as conditions between these two, can be simulated in FASTRAN II by using a constraint factor on tensile yielding at the crack front to approximately account for three-dimensional stress states. FASTRAN II contains seventeen predefined crack configurations (standard laboratory fatigue crack growth rate specimens and many common crack configurations found in structures); and the user can define one additional crack configuration. The baseline crack growth rate properties (effective stress-intensity factor against crack growth rate) may be given in either equation or tabular form. For three-dimensional crack configurations, such as surface cracks or corner cracks at holes or notches, the fatigue crack growth rate properties may be different in the crack depth and crack length directions. Final failure of the cracked structure can be modelled with fracture toughness properties using either linear-elastic fracture mechanics (brittle materials), a two-parameter fracture criterion (brittle to ductile materials), or plastic collapse (extremely ductile materials). The crack configurations in FASTRAN II can be subjected to either constant-amplitude, variable-amplitude or spectrum loading. The applied loads may be either tensile or compressive. Several standardized aircraft flight-load histories, such as TWIST, Mini-TWIST, FALSTAFF, Inverted FALSTAFF, Felix and Gaussian, are included as options. FASTRAN II also includes two other methods that will help the user input spectrum load histories. The two methods are: (1) a list of stress points, and (2) a flight-by-flight history of stress points. Examples are provided in the user manual. Developed as a research program, FASTRAN II has successfully predicted crack growth in many metallic materials under various aircraft spectrum loading. A computer program DKEFF which is a part of the FASTRAN II package was also developed to analyze crack growth rate data from laboratory specimens to obtain the effective stress-intensity factor against crack growth rate relations used in FASTRAN II. FASTRAN II is written in standard FORTRAN 77. It has been successfully compiled and implemented on Sun4 series computers running SunOS and on IBM PC compatibles running MS-DOS using the Lahey F77L FORTRAN compiler. Sample input and output data are included with the FASTRAN II package. The UNIX version requires 660K of RAM for execution. The standard distribution medium for the UNIX version (LAR-14865) is a .25 inch streaming magnetic tape cartridge in UNIX tar format. It is also available on a 3.5 inch diskette in UNIX tar format. The standard distribution medium for the MS-DOS version (LAR-14944) is a 5.25 inch 360K MS-DOS format diskette. The contents of the diskette are compressed using the PKWARE archiving tools. The utility to unarchive the files, PKUNZIP.EXE, is included. The program was developed in 1984 and revised in 1992. Sun4 and SunOS are trademarks of Sun Microsystems, Inc. IBM PC is a trademark of International Business Machines Corp. MS-DOS is a trademark of Microsoft, Inc. F77L is a trademark of the Lahey Computer Systems, Inc. UNIX is a registered trademark of AT&T Bell Laboratories. PKWARE and PKUNZIP are trademarks of PKWare, Inc.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-14944
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  • 90
    Publication Date: 2011-08-24
    Description: The Panel Analysis and Sizing Code (PASCO) was developed for the buckling and vibration analysis and sizing of prismatic structures having an arbitrary cross section. PASCO is primarily intended for analyzing and sizing stiffened panels made of laminated orthotropic materials and is of particular value in analyzing and sizing filamentary composite structures. When used in the analysis mode, PASCO calculates laminate stiffnesses, lamina stress and strains (including the effects of temperature and panel bending), buckling loads, vibration frequencies, and overall panel stiffness. When used in the sizing mode, PASCO adjusts sizing variables to provide a low-mass panel design that carries a set of specified loadings without exceeding buckling or material strength allowables and that meets other design requirements such as upper and lower bounds on sizing variables, upper and lower bounds on overall bending, extensional and shear stiffnesses, and lower bounds on vibration frequencies. Although emphasis in PASCO is placed on flat panels having several identical bays, the only restriction on configuration modeling is that the structure is assumed to be prismatic. In addition, it is assumed that loads and temperatures do not vary along the length of a panel. Because of their wide application in aerospace structures, stiffened panels are readily handled by PASCO. The panel cross section may be composed of an arbitrary assemblage of thin, flat, rectangular plate elements that are connected together along their longitudinal edges. Each plate element consists of a balanced symmetric laminate of any number of layers of orthotropic material. Any group of element widths, layer thicknesses, and layer orientation angles may be selected as sizing variables. Substructuring is available to increase the efficiency of the analysis and to simplify the modeling of complicated structures. The Macintosh version of PASCO includes an interactive, graphic preprocessor called MacPASCO. The main objective of MacPASCO is to make the use of PASCO faster, simpler, and less error-prone. By using a graphical user interface (GUI), MacPASCO simplifies the specification of panel geometry and reduces user input errors, thus making the modeling and analysis of panel designs more efficient. The user draws the initial structural geometry on the computer screen, then uses a combination of graphic and text inputs to: refine the structural geometry, specify information required for analysis such as panel load conditions, and define design variables and constraints for minimum-mass optimization. Composite panel design is an ideal application because the graphical user interface can: serve as a visual aid, eliminate the tedious aspects of text-based input, and eliminate many sources of input errors. The current version of MacPASCO does not implement all the modeling features of PASCO, but has been found to be sufficient for many users. Many difficulties common to text-based inputs are avoided because MacPASCO uses a GUI. First, the graphic displays eliminate syntax errors, like misplaced commas and incorrect command names, because there is no text-based syntax. Second, graphic displays allow the user to see the geometry as it is created and immediately detect and correct any errors. Third, MacPASCO's drawing tools have been designed to avoid modeling errors. Fourth, the graphic displays make revisions to existing structural designs much easier and less error-prone by eliminating the need for the user to conceptualize the text input as geometry. The user can work directly with the geometry displayed on the screen. Finally, MacPASCO automatically generates the correct PASCO input from the geometry displayed on the screen. This input file can be used with any machine version of PASCO to actually perform the analysis and sizing and to output results. The DEC VAX version of PASCO is written in FORTRAN IV for batch execution and has been implemented on a DEC VAX series computer. The Macintosh version of PASCO was developed for Macintosh II series computers with at least 2Mb of RAM running MPW Pascal 3.0 and Language Systems FORTRAN 2.0 under the MPW programming environment. It includes MPW compatible makefiles for compiling the source code. The Macintosh version uses input files compatible with versions of PASCO running on different platforms. MacPASCO is written in Macintosh Programmers Workbench 3.0, MPW Pascal 3.0, and MacAPP 2.0. The Pascal source code is included on the distribution diskette. MacAPP is a development library which is not included. MacPASCO requires a Mac Plus, SE/30, or MacII, IIx, IIcx, IIci, or IIfx running System 6.0 or greater. MacPASCO is System 7.0 compatible. A minimum of 2Mb of RAM is required for execution. The Macintosh version of PASCO is distributed on four 3.5 inch 800K Macintosh format diskettes. The DEC VAX version is distributed on a 9-track 1600 BPI magnetic tape. The PASCO program was developed in 1981, adapted to the DEC VAX in 1983 and to the Macintosh in 1991. MacPASCO was released in 1992.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-14799
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  • 91
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    In:  Other Sources
    Publication Date: 2011-08-24
    Description: PLAN2D is a FORTRAN computer program for the plastic analysis of planar rigid frame structures. Given a structure and loading pattern as input, PLAN2D calculates the ultimate load that the structure can sustain before collapse. Element moments and plastic hinge rotations are calculated for the ultimate load. The location of hinges required for a collapse mechanism to form are also determined. The program proceeds in an iterative series of linear elastic analyses. After each iteration the resulting elastic moments in each member are compared to the reserve plastic moment capacity of that member. The member or members that have moments closest to their reserve capacity will determine the minimum load factor and the site where the next hinge is to be inserted. Next, hinges are inserted and the structural stiffness matrix is reformulated. This cycle is repeated until the structure becomes unstable. At this point the ultimate collapse load is calculated by accumulating the minimum load factor from each previous iteration and multiplying them by the original input loads. PLAN2D is based on the program STAN, originally written by Dr. E.L. Wilson at U.C. Berkeley. PLAN2D has several limitations: 1) Although PLAN2D will detect unloading of hinges it does not contain the capability to remove hinges; 2) PLAN2D does not allow the user to input different positive and negative moment capacities and 3) PLAN2D does not consider the interaction between axial and plastic moment capacity. Axial yielding and buckling is ignored as is the reduction in moment capacity due to axial load. PLAN2D is written in FORTRAN and is machine independent. It has been tested on an IBM PC and a DEC MicroVAX. The program was developed in 1988.
    Keywords: STRUCTURAL MECHANICS
    Type: LEW-14889
    Format: text
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  • 92
    Publication Date: 2011-08-24
    Description: Predictions of fatigue crack growth behavior can be made with the Fatigue Crack Growth Structural Analysis (FASTRAN II) computer program. As cyclic loads are applied to a selected crack configuration with an initial crack size, FASTRAN II predicts crack growth as a function of cyclic load history until either a desired crack size is reached or failure occurs. FASTRAN II is based on plasticity-induced crack-closure behavior of cracks in metallic materials and accounts for load-interaction effects, such as retardation and acceleration, under variable-amplitude loading. The closure model is based on the Dugdale model with modifications to allow plastically deformed material to be left along the crack surfaces as the crack grows. Plane stress and plane strain conditions, as well as conditions between these two, can be simulated in FASTRAN II by using a constraint factor on tensile yielding at the crack front to approximately account for three-dimensional stress states. FASTRAN II contains seventeen predefined crack configurations (standard laboratory fatigue crack growth rate specimens and many common crack configurations found in structures); and the user can define one additional crack configuration. The baseline crack growth rate properties (effective stress-intensity factor against crack growth rate) may be given in either equation or tabular form. For three-dimensional crack configurations, such as surface cracks or corner cracks at holes or notches, the fatigue crack growth rate properties may be different in the crack depth and crack length directions. Final failure of the cracked structure can be modelled with fracture toughness properties using either linear-elastic fracture mechanics (brittle materials), a two-parameter fracture criterion (brittle to ductile materials), or plastic collapse (extremely ductile materials). The crack configurations in FASTRAN II can be subjected to either constant-amplitude, variable-amplitude or spectrum loading. The applied loads may be either tensile or compressive. Several standardized aircraft flight-load histories, such as TWIST, Mini-TWIST, FALSTAFF, Inverted FALSTAFF, Felix and Gaussian, are included as options. FASTRAN II also includes two other methods that will help the user input spectrum load histories. The two methods are: (1) a list of stress points, and (2) a flight-by-flight history of stress points. Examples are provided in the user manual. Developed as a research program, FASTRAN II has successfully predicted crack growth in many metallic materials under various aircraft spectrum loading. A computer program DKEFF which is a part of the FASTRAN II package was also developed to analyze crack growth rate data from laboratory specimens to obtain the effective stress-intensity factor against crack growth rate relations used in FASTRAN II. FASTRAN II is written in standard FORTRAN 77. It has been successfully compiled and implemented on Sun4 series computers running SunOS and on IBM PC compatibles running MS-DOS using the Lahey F77L FORTRAN compiler. Sample input and output data are included with the FASTRAN II package. The UNIX version requires 660K of RAM for execution. The standard distribution medium for the UNIX version (LAR-14865) is a .25 inch streaming magnetic tape cartridge in UNIX tar format. It is also available on a 3.5 inch diskette in UNIX tar format. The standard distribution medium for the MS-DOS version (LAR-14944) is a 5.25 inch 360K MS-DOS format diskette. The contents of the diskette are compressed using the PKWARE archiving tools. The utility to unarchive the files, PKUNZIP.EXE, is included. The program was developed in 1984 and revised in 1992. Sun4 and SunOS are trademarks of Sun Microsystems, Inc. IBM PC is a trademark of International Business Machines Corp. MS-DOS is a trademark of Microsoft, Inc. F77L is a trademark of the Lahey Computer Systems, Inc. UNIX is a registered trademark of AT&T Bell Laboratories. PKWARE and PKUNZIP are trademarks of PKWare, Inc.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-14865
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  • 93
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-24
    Description: The SNIP program is a FORTRAN computer code that generates NASTRAN structural model thermal loads when given SINDA (or similar thermal model) temperature results. SNIP correlates thermal nodes to structural elements to interface SINDA finite difference thermal models with NASTRAN finite element structural models. Node-to-element correlation includes determining which SINDA nodes should be related to each NASTRAN element and calculating a weighing factor for temperatures associated with each element-related thermal node. SNIP provides structural model thermal loads that accurately reflect thermal model results while reducing the time required to interface thermal and structural models as compared to other methods. SNIP uses thermal model geometry to search the three-dimensional space around each structural element for the nearest thermal nodes. Thermal model geometry is the combination of standard thermal model temperature results from SINDA and structural model geometry from NASTRAN. Thermal and structural models must both be defined in the same, single Cartesian coordinate system. The thermal nodes located nearest each element are used to determine element temperature for thermal distortion and stress analysis. The program shapes the three-dimensional search region while the user controls the size. With these region specifications, the numerical coding of thermal nodes, and the structural element numbers; the code can provide for the separation of substructures during correlation. The input to SNIP contains a file of thermal model temperature results and a physical location of each thermal node in three-dimensional space, combined in a SNIP-unique format. The input also contains a standard NASTRAN input deck for a model made up of plate, shell, beam, and bar elements. SNIP supports the CTRIA, CQUAD, CBAR, and CBEAM elements of NASTRAN. The user adjusts the input parameters in the source code which control the node-to-element correlation. The program outputs NASTRAN element temperature load cards for each element and NASTRAN case control cards for each temperature load set. SNIP also outputs a list of elements that contains the numbers of the SINDA nodes related to each NASTRAN element and the weight that is given to each node in temperature calculations. SNIP is written in ANSI standard FORTRAN 77. The PC version requires a PC FORTRAN compiler and has compiled successfully using Lahey FORTRAN v. 3.0. A core memory of 300k is recommended. The program was developed in 1987.
    Keywords: STRUCTURAL MECHANICS
    Type: LEW-14741
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  • 94
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-24
    Description: NPLOT is an interactive computer graphics program for plotting undeformed and deformed NASTRAN finite element models (FEMs). Although there are many commercial codes already available for plotting FEMs, these have limited use due to their cost, speed, and lack of features to view BAR elements. NPLOT was specifically developed to overcome these limitations. On a vector type graphics device the two best ways to show depth are by hidden line plotting or haloed line plotting. A hidden line algorithm generates views of models with all hidden lines removed, and a haloed line algorithm displays views with aft lines broken in order to show depth while keeping the entire model visible. A haloed line algorithm is especially useful for plotting models composed of many line elements and few surface elements. The most important feature of NPLOT is its ability to create both hidden line and haloed line views accurately and much more quickly than with any other existing hidden or haloed line algorithms. NPLOT is also capable of plotting a normal wire frame view to display all lines of a model. NPLOT is able to aid in viewing all elements, but it has special features not generally available for plotting BAR elements. These features include plotting of TRUE LENGTH and NORMALIZED offset vectors and orientation vectors. Standard display operations such as rotation and perspective are possible, but different view planes such as X-Y, Y-Z, and X-Z may also be selected. Another display option is the Z-axis cut which allows a portion of the fore part of the model to be cut away to reveal details of the inside of the model. A zoom function is available to terminals with a locator (graphics cursor, joystick, etc.). The user interface of NPLOT is designed to make the program quick and easy to use. A combination of menus and commands with help menus for detailed information about each command allows experienced users greater speed and efficiency. Once a plot is on the screen the interface becomes command driven, enabling the user to manipulate the display or execute a command without having to return to the menu. NPLOT is also able to plot deformed shapes allowing it to perform post-processing. The program can read displacements, either static displacements or eigenvectors, from a MSC/NASTRAN F06 file or a UAI/NASTRAN PRT file. The displacements are written into a unformatted scratch file where they are available for rapid access when the user wishes to display a deformed shape. All subcases or mode shapes can be read in at once. Then it is easy to enable the deformed shape, to change subcases or mode shapes and to change the scale factor for subsequent plots. NPLOT is written in VAX FORTRAN for DEC VAX series computers running VMS. As distributed, the NPLOT source code makes calls to the DI3000 graphics package from Precision Visuals; however, a set of interface routines is provided to translate the DI3000 calls into Tektronix PLOT10/TCS graphics library calls so that NPLOT can use the standard Tektronix 4010 which many PC terminal emulation software programs support. NPLOT is available in VAX BACKUP format on a 9-track 1600 BPI DEC VAX BACKUP format magnetic tape (standard media) or a TK50 tape cartridge. This program was developed in 1991. DEC, VAX, VMS, and TK50 are trademarks of Digital Equipment Corporation. Tektronix, PLOT10, and TCS are trademarks of Tektronix, Inc. DI3000 is a registered trademark of Precision Visuals, Inc. NASTRAN is a registered trademark of the National Aeronautics and Space Administration. MSC/ is a trademark of MacNeal-Schwendler Corporation. UAI is a trademark of Universal Analytics, Inc.
    Keywords: STRUCTURAL MECHANICS
    Type: GSC-13458
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  • 95
    Publication Date: 2011-08-24
    Description: LATDYN is a computer code for modeling the Large Angle Transient DYNamics of flexible articulating structures and mechanisms involving joints about which members rotate through large angles. LATDYN extends and brings together some of the aspects of Finite Element Structural Analysis, Multi-Body Dynamics, and Control System Analysis; three disciplines that have been historically separate. It combines significant portions of their distinct capabilities into one single analysis tool. The finite element formulation for flexible bodies in LATDYN extends the conventional finite element formulation by using a convected coordinate system for constructing the equation of motion. LATDYN's formulation allows for large displacements and rotations of finite elements subject to the restriction that deformations within each are small. Also, the finite element approach implemented in LATDYN provides a convergent path for checking solutions simply by increasing mesh density. For rigid bodies and joints LATDYN borrows extensively from methodology used in multi-body dynamics where rigid bodies may be defined and connected together through joints (hinges, ball, universal, sliders, etc.). Joints may be modeled either by constraints or by adding joint degrees of freedom. To eliminate error brought about by the separation of structural analysis and control analysis, LATDYN provides symbolic capabilities for modeling control systems which are integrated with the structural dynamic analysis itself. Its command language contains syntactical structures which perform symbolic operations which are also interfaced directly with the finite element structural model, bypassing the modal approximation. Thus, when the dynamic equations representing the structural model are integrated, the equations representing the control system are integrated along with them as a coupled system. This procedure also has the side benefit of enabling a dramatic simplification of the user interface for modeling control systems. Three FORTRAN computer programs, the LATDYN Program, the Preprocessor, and the Postprocessor, make up the collective LATDYN System. The Preprocessor translates user commands into a form which can be used while the LATDYN program provides the computational core. The Postprocessor allows the user to interactively plot and manage a database of LATDYN transient analysis results. It also includes special facilities for modeling control systems and for programming changes to the model which take place during analysis sequence. The documentation includes a Demonstration Problem Manual for the evaluation and verification of results and a Postprocessor guide. Because the program should be viewed as a byproduct of research on technology development, LATDYN's scope is limited. It does not have a wide library of finite elements, and 3-D Graphics are not available. Nevertheless, it does have a measure of "user friendliness". The LATDYN program was developed over a period of several years and was implemented on a CDC NOS/VE & Convex Unix computer. It is written in FORTRAN 77 and has a virtual memory requirement of 1.46 MB. The program was validated on a DEC MICROVAX operating under VMS 5.2.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-14382
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  • 96
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-24
    Description: The increasing number of applications of fiber-reinforced composites in industry demands a detailed understanding of their material properties and behavior. A three-dimensional finite-element computer program called PAFAC (Plastic and Failure Analysis of Composites) has been developed for the elastic-plastic analysis of fiber-reinforced composite materials and structures. The evaluation of stresses and deformations at edges, cut-outs, and joints is essential in understanding the strength and failure for metal-matrix composites since the onset of plastic yielding starts very early in the loading process as compared to the composite's ultimate strength. Such comprehensive analysis can only be achieved by a finite-element program like PAFAC. PAFAC is particularly suited for the analysis of laminated metal-matrix composites. It can model the elastic-plastic behavior of the matrix phase while the fibers remain elastic. Since the PAFAC program uses a three-dimensional element, the program can also model the individual layers of the laminate to account for thickness effects. In PAFAC, the composite is modeled as a continuum reinforced by cylindrical fibers of vanishingly small diameter which occupy a finite volume fraction of the composite. In this way, the essential axial constraint of the phases is retained. Furthermore, the local stress and strain fields are uniform. The PAFAC finite-element solution is obtained using the displacement method. Solution of the nonlinear equilibrium equations is obtained with a Newton-Raphson iteration technique. The elastic-plastic behavior of composites consisting of aligned, continuous elastic filaments and an elastic-plastic matrix is described in terms of the constituent properties, their volume fractions, and mutual constraints between phases indicated by the geometry of the microstructure. The program uses an iterative procedure to determine the overall response of the laminate, then from the overall response determines the stress state in each phase of the composite material. Failure of the fibers or matrix within an element can also be modeled by PAFAC. PAFAC is written in FORTRAN IV for batch execution and has been implemented on a CDC CYBER 170 series computer with a segmented memory requirement of approximately 66K (octal) of 60 bit words. PAFAC was developed in 1982.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-13183
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  • 97
    Publication Date: 2011-08-24
    Description: The Panel Analysis and Sizing Code (PASCO) was developed for the buckling and vibration analysis and sizing of prismatic structures having an arbitrary cross section. PASCO is primarily intended for analyzing and sizing stiffened panels made of laminated orthotropic materials and is of particular value in analyzing and sizing filamentary composite structures. When used in the analysis mode, PASCO calculates laminate stiffnesses, lamina stress and strains (including the effects of temperature and panel bending), buckling loads, vibration frequencies, and overall panel stiffness. When used in the sizing mode, PASCO adjusts sizing variables to provide a low-mass panel design that carries a set of specified loadings without exceeding buckling or material strength allowables and that meets other design requirements such as upper and lower bounds on sizing variables, upper and lower bounds on overall bending, extensional and shear stiffnesses, and lower bounds on vibration frequencies. Although emphasis in PASCO is placed on flat panels having several identical bays, the only restriction on configuration modeling is that the structure is assumed to be prismatic. In addition, it is assumed that loads and temperatures do not vary along the length of a panel. Because of their wide application in aerospace structures, stiffened panels are readily handled by PASCO. The panel cross section may be composed of an arbitrary assemblage of thin, flat, rectangular plate elements that are connected together along their longitudinal edges. Each plate element consists of a balanced symmetric laminate of any number of layers of orthotropic material. Any group of element widths, layer thicknesses, and layer orientation angles may be selected as sizing variables. Substructuring is available to increase the efficiency of the analysis and to simplify the modeling of complicated structures. The Macintosh version of PASCO includes an interactive, graphic preprocessor called MacPASCO. The main objective of MacPASCO is to make the use of PASCO faster, simpler, and less error-prone. By using a graphical user interface (GUI), MacPASCO simplifies the specification of panel geometry and reduces user input errors, thus making the modeling and analysis of panel designs more efficient. The user draws the initial structural geometry on the computer screen, then uses a combination of graphic and text inputs to: refine the structural geometry, specify information required for analysis such as panel load conditions, and define design variables and constraints for minimum-mass optimization. Composite panel design is an ideal application because the graphical user interface can: serve as a visual aid, eliminate the tedious aspects of text-based input, and eliminate many sources of input errors. The current version of MacPASCO does not implement all the modeling features of PASCO, but has been found to be sufficient for many users. Many difficulties common to text-based inputs are avoided because MacPASCO uses a GUI. First, the graphic displays eliminate syntax errors, like misplaced commas and incorrect command names, because there is no text-based syntax. Second, graphic displays allow the user to see the geometry as it is created and immediately detect and correct any errors. Third, MacPASCO's drawing tools have been designed to avoid modeling errors. Fourth, the graphic displays make revisions to existing structural designs much easier and less error-prone by eliminating the need for the user to conceptualize the text input as geometry. The user can work directly with the geometry displayed on the screen. Finally, MacPASCO automatically generates the correct PASCO input from the geometry displayed on the screen. This input file can be used with any machine version of PASCO to actually perform the analysis and sizing and to output results. The DEC VAX version of PASCO is written in FORTRAN IV for batch execution and has been implemented on a DEC VAX series computer. The Macintosh version of PASCO was developed for Macintosh II series computers with at least 2Mb of RAM running MPW Pascal 3.0 and Language Systems FORTRAN 2.0 under the MPW programming environment. It includes MPW compatible makefiles for compiling the source code. The Macintosh version uses input files compatible with versions of PASCO running on different platforms. MacPASCO is written in Macintosh Programmers Workbench 3.0, MPW Pascal 3.0, and MacAPP 2.0. The Pascal source code is included on the distribution diskette. MacAPP is a development library which is not included. MacPASCO requires a Mac Plus, SE/30, or MacII, IIx, IIcx, IIci, or IIfx running System 6.0 or greater. MacPASCO is System 7.0 compatible. A minimum of 2Mb of RAM is required for execution. The Macintosh version of PASCO is distributed on four 3.5 inch 800K Macintosh format diskettes. The DEC VAX version is distributed on a 9-track 1600 BPI magnetic tape. The PASCO program was developed in 1981, adapted to the DEC VAX in 1983 and to the Macintosh in 1991. MacPASCO was released in 1992.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-13164
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  • 98
    Publication Date: 2011-08-24
    Description: BUCKO is a computer program developed to predict the buckling load of a rectangular compression-loaded orthotropic plate with a centrally located cutout. The plate is assumed to be a balanced, symmetric laminate of uniform thickness. The cutout shape can be elliptical, circular, rectangular, or square. The BUCKO package includes sample data that demonstrates the essence of the program and its ease of usage. BUCKO uses an approximate one-dimensional formulation of the classical two-dimensional buckling problem following the Kantorovich method. The boundary conditions are considered to be simply supported unloaded edges and either clamped or simply supported loaded edges. The plate is loaded in uniaxial compression by either uniformly displacing or uniformly stressing two opposite edges of the plate. The BUCKO analysis consists of two parts: calculation of the inplane stress distribution prior to buckling, and calculation of the plate axial load and displacement at buckling. User input includes plate planform and cutout geometry, plate membrane and bending stiffnesses, finite difference parameters, boundary condition data, and loading data. Results generated by BUCKO are the prebuckling strain energy, inplane stress resultants, buckling mode shape, critical end shortening, and average axial and transverse strains at buckling. BUCKO is written in FORTRAN V for batch execution and has been implemented on a CDC CYBER 170 series computer operating under NOS with a central memory requirement of approximately 343K of 60 bit words. This program was developed in 1984 and was last updated in 1990.
    Keywords: STRUCTURAL MECHANICS
    Type: LAR-13466
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  • 99
    Publication Date: 2011-08-24
    Description: A thermoviscoplastic finite element method employing the Bodner-Partom constitutve model is used to investigate the response of simplified thermal-structural models to intense local heating. The computational method formulates the problem in rate and advances the solution in time by numerical integration. The thermoviscoplastic response of simplified structures with prescribed temperatures is investigated. With rapid rises of temperature, the nickel alloy structures display initially higher yield stresses due to strain rate effects. As temperatures approach elevated values, yield stress and stiffness degrade rapidly and pronounced plastic deformation occurs.
    Keywords: STRUCTURAL MECHANICS
    Type: Journal of Aerospace Engineering (ISSN 0893-1321); 7; 1; p. 50-71
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  • 100
    Publication Date: 2011-08-24
    Description: A three-bay, space, cantilever truss is probabilistically evaluated to describe progressive buckling and truss collapse in view of the numerous uncertainties associated with the structural, material, and load variables that describe the truss. Initially, the truss is deterministically analyzed for member forces, and members in which the axial force exceeds the Euler buckling load are identified. These members are then discretized with several intermediate nodes, and a probabilistic buckling analysis is performed on the truss to obtain its probabilistic buckling loads and the respective mode shapes. Furthermore, sensitivities associated with the uncertainties in the primitive variables are investigated, margin of safety values for the truss are determined, and truss end node displacements are noted. These steps are repeated by sequentially removing buckled members until onset of truss collapse is reached. Results show that this procedure yields an optimum truss configuration for a given loading and for a specified reliability.
    Keywords: STRUCTURAL MECHANICS
    Type: Journal of Spacecraft and Rockets (ISSN 0022-4650); 31; 3; p. 466-474
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