Accession Number : ADA952097

Title :   Pressure and Heat Transfer Measurements over a Circular Cylinder at Angles of Attack up to 15 deg at M = 11,

Corporate Author : PRINCETON UNIV NJ JAMES FORRESTAL RESEARCH CENTER

Personal Author(s) : Horstman, C. C.

Report Date : JAN 1963

Pagination or Media Count : 80

Descriptors :   *WIND TUNNEL TESTS, *HYPERSONIC WIND TUNNELS, *CYLINDRICAL BODIES, *PRESSURE DISTRIBUTION, *HEAT TRANSFER, *SWEPTBACK WINGS, AERODYNAMIC CONFIGURATIONS, LEADING EDGES, HYPERSONIC AIRCRAFT, CIRCULAR, ANGLE OF ATTACK, AXISYMMETRIC, INVISCID FLOW, AFTERBODIES, ENTROPY, LAYERS, NOSES, SHAPE, SHOCK WAVES, MACH NUMBER, REYNOLDS NUMBER, FREE STREAM, DATA REDUCTION.

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE