TURBULENT NONISOTHERMAL JETS OF A COMPRESSIBLE GAS OF VARIABLE COMPOSITION.

Abstract

A compressible turbulent jet of variable composition is analyzed using the integral method. The analysis is divided into six parts, with the following assumptions holding throughout: the flow is isobaric, the specific heat of each component in the jet is temperature-independent, pressure and thermal diffusion are neglected, the density is determined from the Clapeyron equation, and there are no chemical reactions. Part 1 treats a plane nonisothermal jet in a wake with Pr sub t = Pr sub d = 1 at high velocities, the governing boundary layer equation, and the energy equation. In Part 2, the same problem is analyzed for an axisymmetric jet. Part 3 is the same as Parts 1 and 2 combined, except that the flow velocity is assumed to be very low. The results of the analysis are shown as velocity profile curves for various radial temperature distributions. In Parts 4-6, the conditions Pr sub t = Pr sub d = 1 are relaxed. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1967
Accession Number
AD0665593

Entities

People

  • A. S. Ginevskii

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axisymmetric
  • Boundaries
  • Boundary Layer
  • Chemical Reactions
  • Diffusion
  • Equations
  • Integrals
  • Layers
  • Lepidoptera
  • Specific Heat
  • Thermal Diffusion

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Materials Science and Engineering.