ASD Technical Report, Numéro 63,Partie 755Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963 |
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Expressions et termes fréquents
0.2 WEDGE SHARP 1.0 ON PLATE 1.0 ON WEDGE 1.6 X SYMBOL AEDC Tunnels angle of attack ASD Technical Documentary Blunt Leading Edge CHORD WISE STATION figure numbers Film Flow Photograph FIN L.E. flat plate surface Grumman Hypersonic Shock Grumman Shock Tunnel HEIGHT STATION Fig HEIGHT STATION Spanwise Heightwise Pressure Data Hypersonic Flow Separation Kaufman L. E. BLUNT L. E. NONDIMENSIONAL CHORD WISE NONDIMENSIONAL HEIGHT STATION NONDIMENSIONAL SEMISPAN STATION numbers per foot Oil Film Flow PLATE Fig PLATE L. E. Pressure and heat Pressure Data Plots Pressure Measurements pressure psia Re/ft Results in Ref SEMISPAN STATION NONDIMENSIONAL separate models SHARP L. E. BLUNT Sharp Leading Edge SMALL WEDGE 0.4 Spanwise and Heightwise STATION NONDIMENSIONAL HEIGHT Streamwise Pressure Data Surface of Model SYMBOL X SYMBOL Technical Documentary Report TEST CONDITIONS tunnel conditions tunnel pressure level Upper Surface WEDGE Fig WEDGE NONDIMENSIONAL SEMISPAN WEDGE SHARP L. E. απ