EXPERIMENTAL DETERMINATION OF PRESSURE DISTRIBUTION OVER SLENDER CONES AT ANGLES OF ATTACK AT MACH 14.
Scientific rept., Aug 63-May 64,
CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING
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Two slender cones, LD 4 and LD 8, were tested at a nominal Mach number of 14 in air. Total pressure and temperature conditions were 1400-1600 psia and 1350-1550F., respectively. Experimental pressure data was obtained for angles of attack between 0-20 degrees and circumferential angles of 0-180 degrees. This data is presented in conjunction with Sims and Newtonian Impact theories. Author
- Fluid Mechanics