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  • Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects [microform] / by Peter J. Paraska.

    • Text
    • Bethesda, MD : Carderock Division, Naval Surface Warfare Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • J-integral estimates for cracks in infinite bodies [microform] / N.E. Dowling.

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

  • Fracture analysis of stiffened panels under biaxial loading with widespread cracking [microform] / J.C. Newman, Jr.

    • 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

  • Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].

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

  • Computational simulation of damage progression of composite thin shells subjected to mechanical loads [microform] / P.K. Gotsis, C.C. Chamis, L. Minnetyan.

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

  • Determination of the ultimate capacity of elastomeric bearings under axial loading [microform] : a report to U.S. Department of Commerce, Technology Administration, National Institute of Standards and Technology, Building and Fire Research Laboratory / Gregory L. Bradley and Peter C. Chang and Andrew W. Taylor.

    • Text
    • Gaithersburg, MD : The Institute, [1998]
    • 1998

  • 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

  • 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

  • Testing and analysis of composite skin/stringer debonding under multi-axial loading [microform] / Ronald Krueger ... [et al.].

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

  • Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells [microform] : presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category / Theodore F. Johnson, Michael F. Card.

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

  • Analysis and design of the NASA Langley cryogenic pressure box [microform] / David E. Glass ... [et al.].

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

  • Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Hanover, Md. : Available from the NASA Center for Aerospace Information, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55251

  • Plate and butt-weld stresses beyond elastic limit, material and structural modeling [microform] / V. Verderaime.

    • 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], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65623

  • Stiffened panels with initial distortions axially loaded to failure / by B. Skjeggestad, E. Bakke.

    • Text
    • Trondheim : Skipsteknisk Forskningsinstitutt, 1966.
    • 1966
    • 1 Item
    FormatCall NumberItem Location
    Text JSF 72-422Offsite

  • Axial and torsional fatigue behavior of Waspaloy / S. Zamrik, M. Mirdamadi, and F. Zahiri.

    • Text
    • University Park, Pa. : Pennsylvania State University, Engineering Science and Mechanics Department ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24985

  • Unit-sphere anisotropic multiaxial stochastic-strength model probability density distribution for the orientation of critical flaws / Noel N. Nemeth.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50521

  • Forced response testing of anaxi-centrifugal turboshaft engine / A. Karl Owen [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Adelphi, Maryland : U.S. Army Research Laboratory, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69828

  • Geosynthetic reinforced soil performance testing--axial load deformation relationships / authors, Nicks, J.E. [and three others].

    • Text
    • McLean, VA : U.S. Department of Transportation, Federal Highway Administration, Research, Development, and Technology, Turner-Fairbank Highway Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo41563

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