PROBING TECHNIQUES FOR USE IN HIGH TEMPERATURE REACTING FLOWS

Abstract

A basic probe has been designed which consists of a 1/8-in.-diam, water-cooled copper probe with an inside diameter of 0.050 in. These probes may be aspirated to take a gas sample and temperature reading, or used without aspiration to measure total pressure. Two systems currently being investigated to measure temperature are quartz-coated thermocouples and pneumatic thermometers. These probe designs were chosen because they should not include the heat of recombination of non-equilibrium gases in the temperature reading as would a calorimeter-type total enthalpy probe. The gases are analyzed on line with a bistable fluid oscillator having an oscillation frequency that is a function of the molecular weight of the sample. No quantitative theory of fluid oscillators is available; however, observations are given of the effect of some of the design parameters on performance. A study was made of the effect of probe shape and Mach number on the validity of samples taken in a supersonic stream. For hydrogen-nitrogen mixtures at a static pressure of 1 atm, no change between the free stream and the sample was seen in any of the tests.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1968
Accession Number
AD0829143

Entities

People

  • R. P. Rhodes

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Barometric Pressure
  • Boundary Layer
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Combustion Products
  • Engineering
  • Fluid Dynamics
  • Frequency
  • Mach Number
  • Measurement
  • Molecular Weight
  • Oscillators
  • Pressure Measurement
  • Static Pressure
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Electronics Engineering
  • Fluid Dynamics.

Technology Areas

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