A METHOD OF CALCULATING TURBULENT-BOUNDARY-LAYER GROWTH AT HYPERSONIC MACH NUMBERS

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1959
Accession Number
AD0208774

Entities

People

  • James C. Sivells
  • Robert G. Payne

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Axisymmetric
  • Boundary Layer
  • Coefficients
  • Conical Nozzles
  • Equations
  • Experimental Data
  • Free Stream
  • Friction
  • Heat Transfer
  • Incompressible Flow
  • Mach Number
  • Momentum
  • Physical Properties
  • Skin Friction
  • Stagnation Temperature
  • Turbulent Boundary Layer
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow