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  • High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test [microform] / Brent R. Cobleigh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Dynamics and statics of nonaxisymmetric liquid bridges [microform] : second annual report ... / prepared by J. Iwan D. Alexander (principal investigator) ... [et al.].

    • Text
    • Huntsville, Ala. : Center for Microgravity and Materials Research, University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Dynamic stability instrumentation system (DSIS) [microform] / T.L. Jordan ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994- ]
    • 1994-present

  • Dynamic response and stability of a composite prop-fan model [microform] / by Arthur F. Smith and Bennett M. Brooks.

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

  • The dynamics and control of large flexible space structures-X. . Part I [microform] : final report / by Peter M. Bainum, principal investigator ... [et al.].

    • Text
    • Washington, D.C. : Dept. of Mechanical Engineering, School of Engineering, Howard University : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Subsonic dynamics of stardust sample return capsule [microform] / R.A. Mitcheltree and C.M. Fremaux.

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

  • Analysis of wind tunnel oscillatory data of the X-31A aircraft [microform] / Mark S. Smith.

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

  • V/STOL dynamics, control, and flying qualities [microform] / James A. Franklin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000

  • Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors [microform] / Raimund Wohlrab.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • SSME LOX post flow analysis/fluid structure interaction [microform]. Volume 1, Flow analysis : final report / by Roger W. Burke.

    • Text
    • Huntsville, AL : Lockheed Missiles and Space Co., Huntsville Engineering Center ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfieldl, Va. : National Technical Information Service, distributor, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61869

  • SSME LOX post flow analysis/fluid structure interaction [microform] : final report.

    • Text
    • Huntsville, AL : Lockheed Missiles & Space Co. ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61869

  • Dynamic characteristics of two 300 Kw class dual keel space station concepts [microform] / John T. Dorsey ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85508

  • Hover test of a full-scale hingeless helicopter rotor [microform] : aeroelastic stability, performance, and loads data / William Warmbrodt, Randall L. Peterson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed / by Arthur F. Smith.

    • Text
    • Windsor Locks, Conn. : Hamilton Standard Division, United Technologies Corporation ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo26015

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