Accession Number : ADA952093

Title :   The Effect of Wall Temperature on Stagnation Region Heat Transfer and Shock Detachment Distance in Hypersonic Incipient Merged Layer Flow,

Corporate Author : PRINCETON UNIV NJ DEPT OF AEROSPACE AND MECHANICAL SCIENCES

Personal Author(s) : Liu, J. T. C.

Report Date : AUG 1965

Pagination or Media Count : 43

Descriptors :   *HYPERSONIC FLOW, *HEAT TRANSFER, STAGNATION TEMPERATURE, WALLS, REYNOLDS NUMBER, SHOCK WAVES.

Subject Categories : Fluid Mechanics
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE