EXPERIMENTAL DETERMINATION OF PRESSURE DISTRIBUTION OVER SLENDER CONES AT ANGLES OF ATTACK AT MACH 14.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1965
- Accession Number
- AD0628549
Entities
People
- Stuart E. Larsen
- Werner Hoelmer
Organizations
- University of Cincinnati