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William E McCain
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Cilt sonuçları
Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces
William E McCain · National Aeronautics and Space Administration, Langley Research Center
Sayfa sayısı yok · 1983
Airplanes / Wings / Oscillating wings (Aerodynamics)