Total Enthalpy Measurement from Blunt Body Gas Cap Emission in Arc-Heated Wind Tunnels: Results and Application

Abstract

At the Air Force Flight Dynamics Laboratory, there has been a continuing program to measure total enthalpy during test conditions in which heating rates are above 5000 BTU/sq ft-sec. Below this level of heating, steady state enthalpy probes and steady state calorimeters can be successfully employed to determine total enthalpy. However, above 5000 BTU/sq ft-sec, in an important region for re-entry testing, the heating is so severe that only 2,3 transient probes can be employed. When using transient probes (calorimeters or enthalpy probes), empirical corrections must be made, and Fay and Riddell's theory must be applied in order to determine total enthalpy. This is complicated by the fact that the enthalpy is not uniform for many test conditions, and may vary across the flow by a factor between 2 and 4. Therefore, the transient probes must have response characteristics of high enough quality to measure an enthalpy distribution, rather than just one value of total enthalpy. This is further complicated by heater unsteadiness effects.

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Document Details

Document Type
Technical Report
Publication Date
Jul 25, 1972
Accession Number
ADA377949

Entities

People

  • J. P. Doyle Jr
  • L. R. Lawrence Jr.
  • R. E. Walterick
  • T. M. Weeks

Organizations

  • Flight Dynamics Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Blunt Bodies
  • Electronic States
  • Electrons
  • Energy
  • Equations
  • Free Electrons
  • Free Stream
  • Frequency
  • Gas Caps
  • Gas Laws
  • Heat Transfer
  • Intensity
  • Measurement
  • Spectra
  • Spectral Lines
  • Steady State

Readers

  • Fluid Dynamics.