EFFECT OF MACH NUMBER ON BOUNDARY-LAYER TRANSITION IN THE PRESENCE OF PRESSURE RISE AND SURFACE ROUGHNESS ON AN OGIVE-CYLINDER BODY WITH COLD WALL CONDITIONS

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Document Details

Document Type
Technical Report
Publication Date
Apr 20, 1956
Accession Number
AD0092661

Entities

People

  • Robert J. Carros

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Boundary Layer Transition
  • Coefficients
  • Flow Fields
  • Free Flight
  • Free Stream
  • Heat Transfer
  • Laminar Boundary Layer
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Screw Threads
  • Surface Roughness
  • Turbulent Flow
  • Wind Tunnels