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:

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:

• (*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