Comparison of Theoretical and Experimental Heat Transfer on a Cooled 20 deg. Cone With a Laminar Boundary Layer at a Mach Number of 2.02

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1950
Accession Number
ADA380431

Entities

People

  • Forrest E. Gowen
  • Richard Scherrer

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Boundary Layer
  • Experimental Data
  • Flow Rate
  • Heat Exchangers
  • Heat Transfer
  • Heat Transfer Coefficients
  • Laminar Boundary Layer
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Reynolds Number
  • Stainless Steel
  • Static Pressure
  • Surface Temperature
  • Temperature Gradients
  • Wind Tunnels