Research Catalog

  • Inverse boundary-layer theory and comparison with experiment / James E. Carter.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978.
    • 1978
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo45483
  • Computer-automated opponent for manned air-to-air combat simulations / Walter W. Hankins III.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1979.
    • 1979-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52188
  • Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / Jim A. Penland, James B. Hallissy, and James L. Dillon.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
    • 1979-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52191
  • Adaptive identification and control of structural dynamics systems using recursive lattice filters / N. Sundararajan, Raymond C. Montgomery, and Jeffrey P. Williams.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1985.
    • 1985-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53001
  • Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Delma C. Freeman, Jr., and Barnard Spencer, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71431
  • Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / David M. Schuster.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2001.
    • 2001-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22955

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