Research Catalog

  • 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
  • Full-scale hingeless rotor performance and loads [microform] / Randall L. Peterson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • New investigation of short wings with lateral jets [microform] / E. Carafoli and N. Camarasescu.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983
  • Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
    • 1980-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52217
  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept / David E. Hahne.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
    • 1997-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65472

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