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

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1954
Accession Number
AD0029319

Entities

People

  • Archibald R. Sinclair
  • K. R. Czarnecki

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Boundary Layer Control
  • Boundary Layer Flow
  • Boundary Layer Transition
  • Carbon Dioxide
  • Fineness Ratio
  • Flow
  • Free Stream
  • Heat Transfer
  • Laminar Boundary Layer
  • Mach Number
  • Parabolic Bodies
  • Pressure Distribution
  • Reynolds Number
  • Surface Temperature
  • Wind Tunnels