TURBULENT BOUNDARY LAYER OF A COMPRESSIBLE GAS

Abstract

The theory of a turbulent boundary layer of a compressible gas is set forth or based on a study of the relative change of the coefficients of friction and heat transfer with growth of the M number, the heat transfer factor and the wall permeability factor b. The existence is shown of a limiting law, corresponding to very large Re numbers and almost full of self-simulation of relative changes of the coefficients of friction and heat transfer. Engineering methods are presented for solving the basic problems of friction and heat transfer in turbulent flow of a gas past a solid body. The theoretical conclusions are compared with experimental data.

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Document Details

Document Type
Technical Report
Publication Date
Oct 25, 1965
Accession Number
AD0625803

Entities

People

  • A. I. Leontev
  • S. S. Kutateladze

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Boundary Layer Flow
  • Critical Temperature
  • Energy
  • Fluid Flow
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hydrodynamics
  • Latent Heat
  • Mechanical Properties
  • Phase Transformations
  • Stratified Fluids
  • Thermal Conductivity
  • Thermodynamics
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.