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  1. 1
    Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /
    by Noonan, Kevin W.
    Published 1980
    Government Document Book
  2. 2
    A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies /
    by Weilmuenster, K. James
    Published 1979
    Government Document Book
  3. 3
    Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
    by Jenkins, Renaldo V.
    Published 1983
    Government Document Book
  4. 4
    A review of some Reynolds number effects related to bodies at high angles of attack /
    by Polhamus, Edward C., 1948-
    Published 1984
    Government Document Book
  5. 5
    High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
    Published 1982
    Government Document Book
  6. 6
    Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /
    by Nugent, Jack
    Published 1987
    Government Document Book
  7. 7
    Mach 6 flow field surveys beneath the forebody of an airbreathing missile /
    by Johnston, Patrick J.
    Published 1986
    Government Document Book
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