AN ANALYSIS OF INITIAL STATIC PRESSURE PROBE MEASUREMENTS IN A LOW-DENSITY HYPERVELOCITY WIND TUNNEL

Abstract

An initial experimental program was previously conducted to study the problems in using static pressure probes for flow calibration purposes in low- density, hypervelocity wind tunnels with continuous flow. This data is reviewed in the light of more recent data on thermal transpiration. Results indicate that such probes may be used for what might be termed secondary calibrations, but care is required in interpreting the results. The present experiment yielded data which are compared to static pressures calculated from impact- pressure probe calibrations.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1963
Accession Number
AD0402935

Entities

People

  • David E. Boylan

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Calibration
  • Dynamics
  • Flow
  • Free Stream
  • Gas Dynamics
  • Government Procurement
  • Governments
  • Instrumentation
  • Low Density
  • Mach Number
  • Measurement
  • Pressure Measurement
  • Static Pressure
  • Temperature Gradients
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow