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

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)

Document Details

Document Type
Technical Report
Publication Date
Jun 06, 1969
Accession Number
AD0857281

Entities

People

  • Arnold Polak
  • Chris A. Kalivretenos

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Axisymmetric
  • Boundaries
  • Boundary Layer
  • Experimental Data
  • Flow
  • Flow Visualization
  • Heat Transfer
  • Layers
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow