Research Catalog

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  • Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid [microform] : synthesis and structure of novel metal sulfur-containing complexes / Stan A. Duraj and Maria T. Andras and Aloysius F. Hepp.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, distributor, 1990]
    • 1990

  • Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Mechanical response of thick laminated beams and plates subject to out-of-plane loading [microform] / C.C. Hiel, H.F. Brinson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Mechanical and thermal buckling analysisi of rectangular sandwich panels under different edge conditions [microform] / William L. Ko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Fiber composite sandwich thermostuctural behavior, computationalsimulation [microform] / C.C. Chamis and R.A. Aiello and P.L.N. Murthy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Composite sandwich structure and method for making same [microform] / inventor, Charles J. Magurany.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A higher-order bending theory for laminated composite and sandwich beams [microform] / Geoffrey M. Cook.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • 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

  • Facesheet wrinkling in sandwich structures [microform] / Robert P. Ley, Weichuan, and Uy Mbanefo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Room temperature and elevated temperature composite sandwich joint testing [microform] / Sandra P. Walker.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure [microform] / R. Keith Bird and Eric K. Hoffman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Development and evaluation of stitched sandwich panels [microform] / Larry E. Stanley and Daniel O. Adams.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods [microform] / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60789

  • An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels [microform] / A.T. Nettles, D.G. Lance, and A.J. Hodge.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65683

  • Fire-retardant decorative inks for aircraft interiors [microform] / D.A. Kourtides, Z. Nir, J. A. Mikroyannidis.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Efficient design and analysis of lightweight reinforced core sandwich and PRSEUS structures / Brett A. Bednarcyk ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24329

  • Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite, and sandwich beams and plates / Alexander Tessler ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28010

  • Cubic zig-zag enrichment of the classical Kirchhoff kinematics for laminated and sandwich plates / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28057

  • Modeled and measured dynamics of a composite beam with periodically varying form core / Randolph H. Cabell ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32153

  • An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / Michael P. Nemeth.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45682

  • Identification of crew-systems interactions and decision related trends / Sharon Monica Jones [and five others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45684

  • Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013-2014.
    • 2013-2014
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51535

  • Acoustically tailored composite rotorcraft fuselage panels / Stephen Hambric [and eight others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo60800

  • Marshall Space Flight Center Faculty Fellowship Program / N.F. Six, program director/compiler.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66101

  • Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures / Robert R. McWithey and Dick M. Royster.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71363

  • Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS72357

  • Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53733

  • Integrated structural/acoustic modeling of heterogeneous panels / Brett A. Bednarcyk [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37231

  • Multiscale fatigue life prediction for composite panels / Brett A. Bednarcyk, Phillip W. Yarrington, Steven M. Arnold.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37240

  • Progressive damage analysis of bonded composite joints / Frank A. Leone, Jr., Donato Girolamo, Carlos G. Dávila.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37682

  • Methods for assessing honeycomb sandwich panel wrinkling failures / Bart F. Zalewski and William B. Dial, Brett A. Bednarcyk.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37870

  • Composite Crew Module (CCM) permeability characterization / Michael T. Kirsch.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41418

  • A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure / A.T. Nettles, W.E. Guin, and C.C. Wolfe.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, January 2022.
    • 2022-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174309

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