Research Catalog

  • V/STOL wind-tunnel testing [microform] / David G. Koenig.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95840
  • Results of S5 CH tests with an ARL (Aerospace Research Laboratory) cascade [microform] / A. Fourmaux.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1984]
    • 1984
  • Fan blade shake test results for the 40- by 80-/80- by 120-foot wind tunnel [microform] / William Warmbrodt and Todd Graham.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984
  • 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
  • Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.

    • Text
    • Washington : National Aeronautics and Space Administration, September 1959.
    • 1959-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo182854
  • A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations / by Ralph P. Bielat.

    • Text
    • Washington : National Aeronautics and Space Administration, December 1960.
    • 1960-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo182856
  • Wind tunnel testing of high-rise buildings : an output of the CTBUH Wind Engineering Working Group / Peter Irwin, Roy Denoon & David Scott.

    • Text
    • Milton Park, Abingdon, Oxon : Routledge, 2013.
    • 2013
    • 1 Item
    FormatCall NumberItem Location
    Text TA654.5 .I78 2013Off-site
  • Some low-speed problems of high-speed aircraft by A. Spence and D. Lean.

    • Text
    • Paris, Advisory Group for Aeronautical Research and Development, 1961.
    • 1961
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-357Off-site
  • Verification of three-dimensional flutter calculations by means of wind-tunnel tests on a flexible model / by R. Destuynder and L. Darovsky (Office National d'Etudes et de Recherches Aerospatiales 29, Avenue de la Division Leclerc, 92 Châtillon, France).

    • Text
    • Paris : Advisory Group for Aeronautical Research and Development, 1966.
    • 1966
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-562Off-site
  • Tunnel-wall effects associated with vtol-stol model testing by R.E. Kuhn and R.L. Naeseth.

    • Text
    • Paris, Advisory Group for Aeronautical Research and Development, 1959.
    • 1959
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-303Off-site

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