Rotational Temperature and Number Density Measurements of N2, O2, CO, and CO2 in a Hypersonic Flow Field Using Laser-Raman Spectroscopy

Abstract

After successful laboratory measurements of the rotational temperature T(R) of N2, O2, CO, and CO2 at atmospheric pressure and room temperature and of N2 at 296, 215, and 163 K at an equivalent room temperature pressure of 10 torr, measurements of the rotational temperature of these gases were made in the hypersonic flow field produced by either a sonic orifice or a conical nozzle expansion. Radial profile measurements of T(R) were performed at two axial positions for the N2 nozzle flow field at a reservoir pressure of 10 atm. Agreement was obtained with the electron beam results of Beylich using appropriate reservoir scaling laws. The axial variation of N2 number density was determined for the nozzle source over a range of reservoir pressures (3.3 to 10 atm), and radial profiles at two axial locations were determined for the 10- atm condition. Agreement with the MOC calculations was excellent.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1975
Accession Number
ADA012877

Entities

People

  • J. L. Lewis
  • W. D. Williams

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Electron Beams
  • Engineering
  • Equations
  • Flow
  • Flow Fields
  • Free Stream
  • Gas Flow
  • Generators
  • Laser Beams
  • Lasers
  • Measurement
  • Numerical Analysis
  • Radiation
  • Raman Scattering
  • Scattering
  • Spectra

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Molecular Photonics/Laser Physics

Technology Areas

  • Directed Energy
  • Directed Energy - Lasers
  • Hypersonics
  • Hypersonics - Hypersonic Flow
  • Microelectronics