Accession Number : AD0857281

Title :   Hypersonic-Turbulent Boundary-Layer Separation over a Cone-Cylinder-Flare Configuration,

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : Polak, Arnold ; Kalivretenos, Chris A.

Report Date : 06 JUN 1969

Pagination or Media Count : 32

Abstract : Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data were obtained for a cone-cylinder-flare configuration. The experimental data were correlated with a theoretical prediction. (Author)

Descriptors :   (*CONICAL BODIES, FLOW SEPARATION), (*TURBULENT BOUNDARY LAYER, HYPERSONIC CHARACTERISTICS), CYLINDRICAL BODIES, AERODYNAMIC CONFIGURATIONS, REYNOLDS NUMBER, PRESSURE, DISTRIBUTION, HEAT TRANSFER, FLOW VISUALIZATION.

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE