Experimental Investigation of Heat Transfer through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1952
Accession Number
ADA380476

Entities

People

  • Ellis G. Slack

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Experimental Data
  • Flat Plate Models
  • Free Stream
  • Heat Transfer
  • Heat Transfer Coefficients
  • Laminar Boundary Layer
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Reynolds Number
  • Stagnation Pressure
  • Stagnation Temperature
  • Surface Temperature
  • Temperature Gradients
  • Turbulent Boundary Layer