Accession Number : AD0628549

Title :   EXPERIMENTAL DETERMINATION OF PRESSURE DISTRIBUTION OVER SLENDER CONES AT ANGLES OF ATTACK AT MACH 14.

Descriptive Note : Scientific rept., Aug 63-May 64,

Corporate Author : CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING

Personal Author(s) : Larsen,Stuart E. ; Hoelmer,Werner

Report Date : DEC 1965

Pagination or Media Count : 48

Abstract : Two slender cones, L/D = 4 and L/D = 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)

Descriptors :   (*CONICAL BODIES, HYPERSONIC FLOW), (*HYPERSONIC FLOW, CONICAL BODIES), SLENDER BODIES, AERODYNAMIC LOADING, PRESSURE, DISTRIBUTION, AERODYNAMICS, HYPERSONIC WIND TUNNELS, MODEL TESTS

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE