A THEORETICAL INVESTIGATION OF TURBULENT BOUNDARY LAYER FLOW WITH HEAT TRANSFER AT SUPERSONIC AND HYPERSONIC SPEEDS

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Document Details

Document Type
Technical Report
Publication Date
May 19, 1955
Accession Number
AD0075320

Entities

People

  • Jerome Persh

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Coefficients
  • Computational Fluid Dynamics
  • Equations
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Heat Transfer
  • Hydrodynamics
  • Incompressible Flow
  • Jet Propulsion
  • Mach Number
  • Mechanics
  • Munitions
  • Physics
  • Physics Laboratories
  • Reynolds Number

Technology Areas

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