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a warner robins
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Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards
A. Warner Robins · National Aeronautics and Space Administration, Scientific and Technical Information Office
56 sayfa · 1979
Hypersonic planes / Stability of airplanes
Supersonic wings with significant leading-edge thrust at cruise
A. Warner Robins · For sale by the National Technical Information Service]
25 sayfa · 1980
Aerodynamics, Supersonic / Airplanes / Leading edges (Aerodynamics) / Supersonic Aerodynamics / Wings