THEORY OF A PROBE FOR MEASURING LOCAL ATOM CONCENTRATIONS IN HYPERSONIC DISSOCIATED FLOWS AT LOW DENSITIES

Abstract

The theory of a probe to measure local atom concentrations in hypersonic flows of a dissociated gas at low densities is presented. The probe operates on a principle of measuring the differential heat transfer between catalytic and noncatalytic gages immediately adjacent to one another on the stagnation line of a cylindrical model. The theoretical performance of the probe in the free molecule, the viscous shock-layer, AND THE BOUNDARY-LAYER REGIMES, RESPECTIVELY, IS CONSIDERED. It is shown that the probe cannot be operated successfully in the free-molecule regime, except under unusual circumstances. In continuum flow, it is shown that under those conditions necessary for the atoms in the free stream to reach the surface of the probe (chemically frozen shock layer and boundary layer), we are always working in the viscous shock-layer regime. Accordingly, it is this flow regime in which the probe measurements can be interpreted readily. The results of detailed calculations which relate to the application of this probe to measure local atom concentrations in nonequilibrium, hypersonic nozzle flows are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 09, 1962
Accession Number
AD0276100

Entities

People

  • R.a. Hartuiian

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Flow
  • Free Stream
  • Heat Transfer
  • Hypersonic Flow
  • Hypersonic Nozzles
  • Layers
  • Low Density
  • Measurement
  • Molecules
  • Nozzles
  • Physical Properties

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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