Research Catalog

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  • Benefits of force limiting vibration testing [microform] / Mark E. McNelis, Terry D. Scharton.

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

  • Modal forced vibration analysis of aerodynamically excited turbosystems [microform] : final report / V. Elchuri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1995

  • NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems [microform] : final report / V. Elchuri, P.R. Pamidi.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Component mode synthesis and large deflection vibration of complex structures [microform] : final report for the period ended January 31, 1987 / Chuh Mei, principal investigator and Mo-How Shen.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A study of internal and distributed damping for vibrating turbomachiner blades [microform] / Arthur W. Leissa.

    • Text
    • Columbus, OH : Ohio State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Vibrational control of a nonlinear elastic panel [microform] / P.L. Chow, L. Maestrello.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Euler flow computations on non-matching unstructured meshes [microform] / Udayan Gumaste.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • An experimental and computational investigation of oscillating airfoil unsteady aerodynamics at large mean incidence [microform] / Vincent R. Capece, Max F. Platzer.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55219

  • Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme [microform] / Dennis L. Huff, Timothy W. Swafford, and T.S.R. Reddy.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58957

  • Vibration and flutter of mistuned bladed-disk assemblies [microform] / Krishna Rao V. Kaza and Robert E. Kielb.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • The influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades / F. Sisto and A.T. Chang.

    • Text
    • Hoboken, N.J. : Department of Mechanical Engineering, Stevens Institute of Technology ; Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration, 1983.
    • 1983
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46856

  • The influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades / F. Sisto and A.T. Chang.

    • Text
    • Hoboken, N.J. : Department of Mechanical Engineering, Stevens Institute of Technology ; Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration, 1983.
    • 1983

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