Accession Number : AD0125709

Title :   A THEORETICAL INVESTIGATION OF THE EFFECT ON INJECTION OF AIR ON TURBULENT BOUNDARY LAYER SKIN-FRICTION AND HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC AND HYPERSONIC SPEEDS

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : PERSH, JEROME

Report Date : 04 JAN 1957

Pagination or Media Count : 72

Descriptors :   *AERODYNAMIC HEATING, *TURBULENT BOUNDARY LAYER, HEAT TRANSFER, HYPERSONIC CHARACTERISTICS, REDUCTION, SUPERSONIC FLOW.

Distribution Statement : APPROVED FOR PUBLIC RELEASE