An Experimental Investigation of the Separation of a Hypersonic Boundary Layer on a Flat Plate. Part 1. Pressure Distribution and Optical Studies at M = 11.7

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
ADA951988

Entities

People

  • I. E. Vas
  • W. J. Graham

Organizations

  • Princeton University

Tags

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Air Force
  • Boundary Layer
  • Engineering
  • Flow
  • Flow Fields
  • Free Stream
  • Gas Dynamics
  • Heat Transfer
  • Hypersonic Flow
  • Layers
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Test Facilities
  • Universities

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers