Base drag of body in supersonic flight contributes large percentage of total drag, and this base drag is integrated under pressure acting on base; series of experiments measuring pressures acting on base of missile in free flight at supersonic velocities; results represent values actually measured in flight under full scale conditions as continuous function of Mach number.
Base pressures at supersonic velocities
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 16 , n 3
1949
8 pages
Aufsatz (Zeitschrift)
Englisch
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Axisymmetric Supersonic Turbulent Base Pressures
AIAA | 1978
|Base pressures in supersonic flow
TIBKAT | 1956
|Analysis of base pressure at supersonic velocities and comparison with experiment
Engineering Index Backfile | 1950
|Analysis of base pressure at supersonic velocities and comparison with experiment
Engineering Index Backfile | 1951
|