Research Catalog

  • Residual strength analyses of riveted lap-splice joints [microform] / B.R. Seshadri and J.C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
    • 2000
  • Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading [microform] / Gregory R. Wichorek and John H. Crews, Jr.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986
  • Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S [microform] / Jennifer L. Miller, Marc A. Portanova, W. Steven Johnson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Damage tolerance in filament-wound graphite/epoxy pressure vessels [microform] : final report / William E. Simon, principal investigator, Vinh D. Nguyen, research associate, Ravi K. Chenna, research assistant.

    • Text
    • Beaumont, Tex. : Lamar University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures [microform] / C.E. Harris, J.H. Starnes, Jr., and J.C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Stressed oxidation of C/SiC composites [microform] / Michael C. Halbig ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Determination of residual stress in composite materials using ultrasonic waves [microform] : NASA contract # NAG3-1716 / principal investigator, S.I. Rokhlin.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • A progressive damage methodology for residual strength predictions of center-crack tension composite panels [microform] / Timothy William Coats.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading [microform] / : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / David M. McGowan and Damodar R. Ambur.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure [microform] / C.E. Harris ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • A progressive damage methodology for residual strength predictions of notched composite panels [microform] / Timothy W. Coats and Charles E. Harris.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998
  • Progressive damage analysis of laminated composite (PDALC) [microform] : (a computational model implemented in the NASA COMET finite element code) version 2.0 / Timothy W. Coats ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Isothermal fatigue, damage accumulation, and life prediction of a woven PMC [microform] / Andrew L. Gyekenyesi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Progressive Damage Analysis of Laminated Composite (PDALC)--a computational model implemented in the NASA COMET finite element code [microform] / David C. Lo ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads [microform] / James H. Starnes, Jr. ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case [microform] / C.C. Poe, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58426
  • Boeing/NASA composite components flight service evaluation [microform] / Randy L. Coggeshall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67932
  • Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate [microform] / C.C. Poe, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67347
  • Estimating the R-Curve from residual strength data [microform] / Thomas W. Orange.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985
  • Long-term environmental effects and flight service evaluation of composite materials [microform] / H. Benson Dexter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92351
  • Simulation studies for surfaces and materials strength [electronic resource] : semiannual progress report for cooperative agreement NCC2-297 for the period November 1, 1986 - April 30, 1987 / prepared by Eloret Institute ; Timur Halicioglu ; principal investigator.

    • Text
    • Palo Alto, CA : Eloret Instititute ; Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS114001
  • Simulation studies for surfaces and materials strength [microform] : semiannual progress report for cooperative agreement NCC2-297 for the period November 1, 1986 - April 30, 1987 / prepared by Eloret Institute ; Timur Halicioglu ; principal investigator.

    • Text
    • Palo Alto, CA : Eloret Instititute ; Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS114001
  • A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24323
  • Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code / David C. Lo [and three others]

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65365
  • Stressed oxidation of C/SiC composites / Michael C. Halbig [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72612
  • Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure / C.E. Harris [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67204
  • A progressive damage methodology for residual strength predictions of notched composite panels / Timothy W. Coats and Charles E. Harris.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1998.
    • 1998-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83019
  • Residual strength analyses of riveted lap-splice joints / B.R. Seshadri and J.C Newman, Jr.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2000.
    • 2000-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86047

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