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