Research Catalog

  • Strain rate dependent modeling of polymer matrix composites [microform] / Robert K. Goldberg, Donald C. Stouffer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Influence of ply waviness on fatigue life of tapered composite flexbeam laminates [microform] / Gretchen B. Murri.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • Use of photostress to analyze behavior of an aft skirt test specimen [microform] / prepared by S.C. Gambrell, Jr.

    • Text
    • Tuscaloosa, Ala. : The University of Alabama, College of Engineering, Bureau of Engineering Research ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Center, distributor, 1994]
    • 1994
  • Treatment of singularities in cracked bodies [microform] / K.N. Shivakumar and I.S. Raju.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va., : National Technical Information Service, distributor, 1989]
    • 1989
  • Improvements to a method for the geometrically nonlinear analysis of compressively loaded stiffened composite panels [microform] : progress report for the period July 1991 to December 1991.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Center, distributor, 1991]
    • 1991
  • An evaluation of a coupled microstructural approach for the analysis of functionally graded composites via the finite-element method [microform] / Marek-Jerzy Pindera and Patrick Dunn.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy [microform] / Alan T. Nettles.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • U-groove aluminum weld strength improvement [microform] / V. Verderaime and R. Vaughan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box [microform] / John T. Wang ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Property evaluation of LTM25 composite materials [microform] / A.S. Postyn and C.H. Shah.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Determination of yield in Inconel 718 for axial-torsional loading at temperatures up to 649⁰C [microform] / Christopher M. Gil and Cliff J. Lissenden, Bradley A. Lerch.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998
  • Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.

    • Text
    • Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, DC] : [National Aeronautics and Space Administration], [1984]
    • 1984
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51595
  • Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.

    • Text
    • Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, District of Columbia] : [National Aeronautics and Space Administration], [1984]
    • 1984
  • Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2013.
    • 2013-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49705
  • U-groove aluminum weld strength improvement / V. Verderaime and R. Vaughan.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78956
  • Curved displacement transfer functions for geometric nonlinear large deformation structure shape predictions / William L. Ko, and Van Tran Fleischer, Shun-Fat Lung.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79532
  • Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test / Christine V. Jutte [and five others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo34104
  • Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37308

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