CALCULATION OF TURBULENT HEAT EXCHANGE ON A SEMIPERMEATED SURFACE WHEN A FOREIGN GAS IS BLOWN IN (K RASCHETU TURBULENTNOGO TENLOOBMENA NA POLUPRONITSAEMOI POVERKHNOSTI PRI VDUVE INORODNOGO GAZA),

Abstract

A method is presented for calculating the heat transfer on a semipermeable surface under conditions of subsonic flow with foreign gas injection. The method is based on the solution of the energy equation and the use of the asymptotic theory of the turbulent boundary layer. The obtained results show that the rate of injected gas is only slightly affected by the physical properties of injected and main gases. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 20, 1967
Accession Number
AD0674398

Entities

People

  • A. I. Leontev
  • B. P. Mironov
  • S. S. Kutateladze

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Conductivity
  • Energy
  • Equations
  • Flow
  • Heat Transfer
  • Layers
  • Physical Properties
  • Subsonic Flow
  • Thermophysical Properties
  • Transport Properties
  • Turbulent Boundary Layer

Readers

  • Fluid Dynamics.
  • Information Retrieval