Research Catalog

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  • Three point lead screw positioning apparatus [microform] / inventor, Frank S. Calco.

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

  • Equivalent plate analysis of aircraft wing box structures with general planform geometry [microform] / Gary L. Giles.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85490

  • The construction of airfoil pressure models by the bonded plate method [microform] : achievements, current research, technology development and potential applications / Pierce L. Lawing.

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

  • Contact stresses in pin-loaded orthotropic plates [microform] / M. W. Hyer, E. C. Klang.

    • Text
    • Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Hampton, Va. : National Aeronautics and Space Administration, Applied Materials Branch, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS87558

  • Surface cracks in a plate of finite width under tension or bending [microform] / F. Erdogan and H. Boduroglu.

    • Text
    • Bethlehem, Pa. : Lehigh University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • The modeling of piezoceramic patch interactions with shells, plates and beams [microform] / H.T. Banks, R.C. Smith.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Institute for Computer Applications in Science and Engineering, Langley Research Center, [1992]
    • 1992
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97953

  • A three-node C̊ element for analysis of laminated composite sandwich shells [microform] / C. Wayne Martin, S.F. Lung, and K.K. Gupta.

    • 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, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96605

  • Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [electronic resource] / Anthony Waas and Charles Babcock, Jr.

    • Text
    • Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112451

  • Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutout [microform] / Anthony Waas and Charles Babcock, Jr.

    • Text
    • Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ; [Washington, D.C.? : National Aeronautics and Space Administration, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112451

  • Experimental assessment of advanced Stirling component concepts [microform] / B. Ziph ; prepared for National Aeronautics and Space Administration, Lewis Research Center for U.S. Department of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D. under interagency agreement DE-A101-77CS51040.

    • Text
    • Ann Arbor, MI. : Stirling Thermal Motors, Inc. ; Washington, D.C. : U.S. Dept. of Energy, [1985]
    • 1985

  • Plates and shells containing a surface crack under general loading conditions [microform] / Paul F. Joseph and Fazil Erdogan.

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

  • 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

  • Conditions for symmetries in the buckle patterns of laminated-composite 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/gpo30943

  • On hybrid and mixed finite element methods / Th. H.H. Pian.

    • Text
    • Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
    • 1981
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46542

  • On hybrid and mixed finite element methods / Th. H.H. Pian.

    • Text
    • Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
    • 1981

  • Finite element analysis of composite joint configurations with gaps and overlaps / Ronald Krueger.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2014.
    • 2014-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54829

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