Study of the Pressure Rise Across Shock Waves Required to Separate Laminar and Turbulent Boundary Layers

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1952
Accession Number
ADA378189

Entities

People

  • Coleman Dup. Donaldson
  • Roy H. Lange

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Experimental Data
  • Flow
  • Laminar Boundary Layer
  • Laminar Flow
  • Layers
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Shock Waves
  • Skin Friction
  • Supersonic Diffusers
  • Test Facilities
  • Turbulent Boundary Layer
  • Vortex Generators
  • Wind Tunnels