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