AN EXTENSION OF THE EFFECTS OF HEAT TRANSFER ON BOUNDARY-LAYER TRANSITION ON A PARABOLIC BODY OF REVOLUTION (NACA RM-10) AT A MACH NUMBER OF 1.61

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0029317

Entities

People

  • Archibald R. Sinclair
  • K. R. Czarnecki

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Bodies
  • Boundary Layer
  • Boundary Layer Control
  • Boundary Layer Transition
  • Dew Point
  • Free Stream
  • Heat Transfer
  • Laminar Boundary Layer
  • Laminar Flow
  • Mach Number
  • Parabolic Bodies
  • Pressure Measurement
  • Reynolds Number
  • Skin Friction
  • Surface Properties
  • Surface Roughness