Pressure Measurements on Five Miniature Mach/Flow Angularity Probes at Mach Numbers 1.76, 2.0, 3.0 and 5.0

Abstract

Pressure measurements were obtained on five miniature Mach/flow angularity (MFA) probes which were developed at AEDC as part of an on-going probe development effort. These measurements will be correlated with Mach number and known flow angle in order to calibrate these probes. Secondary objectives were to test a hot-film anemometer and three pitot acoustic probes for durability, and to examine the response of three ported dynamic pressure transducers located downstream of the tunnel test section.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1983
Accession Number
ADA162018

Entities

People

  • E. J. Marquart
  • J. C. Donaldson
  • M. T. Byers
  • S. A. Stepanek

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Anemometers
  • Classification
  • Data Reduction
  • Dynamic Pressure
  • Free Stream
  • Instrumentation
  • Mach Number
  • Measurement
  • Measuring Instruments
  • Pressure Measurement
  • Pressure Transducers
  • Security
  • Static Pressure
  • Test Facilities
  • Transducers
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design