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):
Report Date:
1965-12-01
Pagination or Media Count:
48.0
Abstract:
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
Descriptors:
Subject Categories:
- Fluid Mechanics