THERMAL RECOVERY FACTORS IN SUPERSONIC FLOWS OF GAS MIXTURES.

Abstract

Thermal recovery factors were measured at the stagnation point of a hemispheric probe in low density supersonic jets of helium-argon and hydrogen-nitrogen mixtures. A 'guard' heater in the probe made it possible to eliminate conduction losses. Radiation corrections were small. The final values correspond to adiabatic conditions. With jets of mixed gases the experimental recovery factors were as high as 1.6, substantially above the free molecule limit for pure gases. It is suggested that these anomalously high values are due to the species separation which occurs during the stagnation process and which results in concentrations of heavy species in the stagnation zone higher than in the free stream. The results are correlated in terms of the degree of rarefaction and the composition of the source gas. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1969
Accession Number
AD0691447

Entities

People

  • George Maise
  • John B. Fenn

Organizations

  • Purdue University

Tags

DTIC Thesaurus Topics

  • Adiabatic Conditions
  • Cooperation
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Free Stream
  • Hydrogen
  • Low Density
  • Molecules
  • Nitrogen
  • Radiation
  • Rarefaction
  • Recovery
  • Stagnation Point
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow