Accession Number:

AD0857281

Title:

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

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s):

• Polak, Arnold
• Kalivretenos, Chris A.

Report Date:

1969-06-06

Pagination or Media Count:

32.0

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