Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Die Knickfestigkeit eines Stabes mit elastischer Querstützung.

    • Text
    • Berlin, Wilhelm Ernst & Sohn, 1906.
    • 1906
    • 1 Item
    FormatCall NumberItem Location
    Text OAI p.v. 187 no. 1-6Schwarzman Building - General Research Room 315
    Request for On-site UseRequest Scan

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Knickfestigkeit der Stabverbindungen.

    • Text
    • Berlin, Verlag von Wilhelm Ernst & Sohn, 1925.
    • 1925
    • 1 Item
    FormatCall NumberItem Location
    Text VBA+ p.v. 137 no. 1-13Schwarzman Building - General Research Room 315
    Request for On-site UseRequest Scan

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Stability analysis of plates and shells [microform] : a collection of papers in honor of Dr. Manuel Stein / compiled by Norman F. Knight, Jr., Michael P. Nemeth.

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

  • Probabilistic assessment of uncertain adaptive hybrid composites [microform] / Michael C. Shiao and Surendra N. Singhal and Christos C. Chamis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses [microform] / Govid Rengaranjan, Mohammad A. Aminpour, Norman F. Knight.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Cabin-fuselage-wing structural design concept with engine installation [microform].

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

  • Research in Structures, Structural Dynamics and Materials, 1990 [microform] : work-in-progress papers presented at the AIAA/ASME/ASCE/AHS/ASC 31st Structures, Structural Dynamics and Materials Conference held in Long Beach , California, April 2-4, 1990 / compiled by Jean-Francois M. Barthelemy, Ahmed K. Noor.

    • Text
    • [Washington, DC] : 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

  • 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

  • The buckling response of symmetrically laminated composite plates having a trapezoidal planform area [microform] / H.D. Radloff II, M.W. Hyer, M.P. Nemeth.

    • Text
    • Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating [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

  • Shear buckling analysis of a hat-stiffened panel [microform] / William L. Ko and Raymond H. Jackson.

    • 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

  • Shear buckling of specially orthotropic plates with centrally located cutouts [microform] / Eric C. Klang, Vicki Owen.

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

  • Buckling of composite beams [microform] : CDDF final report : project no. 91-20 / P. Thompson.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates [microform] : an annual progress report / prepared by E. Gail Guynn, Walter L. Bradley.

    • Text
    • College Station, Tex. : Center for Mechanics of Composites, Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1989

  • Active control of buckling of flexible beams [microform] / A. Baz and L. Tampe.

    • Text
    • Washington, DC : Catholic University of America, Mechanical Engineering Dept. : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • The dynamic aspects of thermo-elasto-viscoplastic snap-through and creep buckling phenomena [microform] / by R. Riff and G.J. Simitses.

    • Text
    • [Cleveland, Ohio? : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • User manual for BUNVIS-RG [microform] : an exact buckling and vibration program for lattice structures, with repetitive geometry and substructuring options / M.S. Anderson ... [et al].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders [microform] / Dawn C. Jegley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications [microform] / D.R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels [microform] / Navin Jaunky and Norman F. Knight, Jr., Damodar R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Dynamic delamination buckling in composite laminates under impact loading [microform] : computational simulation / Joseph E. Grady, Christos C. Chamis, and Robert A. Aiello ; prepared for the Second Symposium on Composite Materials, Fatigue and Fracture, sponsored by the American Society for Testing and Materials, Cincinnati, Ohio, April 26-30, 1987.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, [1987]
    • 1987

  • Optimization of composite box-beam structures including effects of subcomponent interaction / Scott A. Ragon, Zafer Gürdal, James H. Starnes, Jr.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Buckling behavior of long anisotropic plates subjected to combined loads [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads [microform] / Michael P. Nemeth.

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

  • Probabilistic assessment of National Wind Tunnel [microform] / A.R. Shah and M. Shiao, C.C. Chamis.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Buckling behavior of long anisotropic plates subjected to combined loads [microform] / Michael P. Nemeth.

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

  • Torsional buckling tests of a simulated solar array [microform] : a final report, grant no. NAG5-2924, June 1, 1995-August 31, 1996 / submitted by E.A. Thornton.

    • Text
    • Charlottesville, VA : School of Engineering & Applied Science, University of Virginia ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Novel composites for wing and fuselage applications [microform] : Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784 / Dave Sharp and Larry Sobel.

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

  • Buckling and postbuckling behavior of laminated composite plates with a cutout [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Nonlinear analysis of the space shuttle superlightweight external fuel tank [microform] / Michael P. Nemeth ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Buckling analysis of anisotropic curved panels and shells with variable curvature [microform] / Navin Jaunky and Norman F. Knight, Jr.; Damodar R. Ambur.

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

  • Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects [microform] / David M. McGowan.

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

  • Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : Dryden Flight Research Center, National Aeronautics and Space Administration ; Linthicum Heights, MD : Available from NASA Center for AeroSpace Information, [1998]
    • 1998

  • Progressive failure studies of composite panels with and without cutouts [microform] / Navin Jaunky ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39065

  • Research in structures, structural dynamics, and materials, 1989 [microform] : work-in-progress and other special presentation papers presented at the AIAA/ASME/ASCE/AHS/ASC 30th Structures, Structural Dynamics, and Materials Conference held in Mobile, Alabama, April 3-5, 1989 / compiled by William F. Hunter, Ahmed K. Noor.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54339

  • Measure of displacement around holes in composite plates subjected to quasi-static compression [microform] / John C. Duke, Jr., ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Compression failure mechanisms of composite structures [microform] / H. Thomas Hahn, Mohsen Sohi, and Suresh Moon.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects [microform] / Manuel Stein, P. Daniel Sydow, and Liviu Librescu.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58822

  • Design guide for predicting nonlinear random response (including snap-through) of buckled plates [microform] / Chung Fai Ng.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Informaton Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61247

  • The use of Lanczos's method to solve the large generalized symmetric definite eigenvalue problem in parallel [microform] / Mark T. Jones, Merrell L. Patrick.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS63961

  • Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts [microform] / Michael P. Nemeth.

    • 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/LPS65434

  • Modal interaction in postbuckled plates [microform] : theory / Gaylen A. Thurston.

    • 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], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65618

  • Innovative design of composite structures [microform] : the use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes / M.W. Hyer, H.H. Lee.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67540

  • Innovative design of composite structures [microform] : the use of curvilinear fiber format in composite structure design / M.W. Hyer, R.F. Charette.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67541

  • Structural behavior of composites with progressive fracture [microform] / Levon Minnetyan, Christos C. Chamis, and Pappu L.N. Murthy.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68983

  • Short-wavelength buckling and shear failures for compression-loaded composite laminates [microform] / Mark J. Shuart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85692

  • Effects of thickness and ply orientation on buckling of laminated plates [microform] / Dawn C. Jegley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85524

  • Buckling of a sublaminate in a quasi-isotropic composite laminate [microform] / K. N. Shivakumar, J. D. Whitcomb.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Stability, vibration, and passive damping of partially restrained imperfect columns [microform] / Zia Razzaq ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95187

  • Analytical results for postbuckling behavior of plates in compression and in shear [microform] / Manuel Stein.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta