ON THE ASSUMPTION OF SPECIFIC-HEAT RATIO NEAR ONE IN THE THEORY OF HIGH-ENERGY GAS FLOWS,

Abstract

The assumption that the ratio of specific heats is near one is of dominant importance in real-gas flow theory for hypersonic shock layers, scaling for dissociating flows, local similarity of the hypersonic boundary layer, and the theory of weak disturbances of a highly excited gas. Certain of these problems are briefly reviewed, chiefly to explain the advantages conferred by this assumption which, though poor a priori, has the power to unify diverse problems, often with surprising accuracy. Special attention is paid to the real-gas theory of sound waves, showing how a reduction of order is achieved for any process of energy release coupled with a state variable. Dispersal by chemical relaxation and by radiative transfer are described as examples. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1964
Accession Number
AD0608593

Entities

People

  • F. K. Moore

Organizations

  • Calspan

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Acoustic Propagation
  • Acoustic Waves
  • Boundaries
  • Boundary Layer
  • Energy
  • Flow
  • Gas Flow
  • High Energy
  • Layers
  • Radiative Transfer
  • Sound Waves
  • Specific Heat
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight