A New Heat Transfer Capability for Application in Hypersonic Flow Using Multiple Schmidt-Boelter Gages

Abstract

Heat transfer measurements were made on a complex scaled wind tunnel model containing 400 miniature discrete sensors in Hypersonic Wind Tunnels B and C at the Arnold Engineering Development Center (AEDC). This test program was significant for a number of reasons which, when combined, have led to the development of a new test capability at the AEDC. First and foremost is the large number of simultaneous thermal measurements made on the wind tunnel test model. The large number of simultaneous measurements on a single test model was primarily driven by the customer's desire to conduct the test program in the most cost effective manner. This request was translated into a system to obtain high quality test data points in the least amount of air on time and to make heat transfer measurements on all surfaces of a very complex model. The measurements were made on relatively flat surfaces, wing leading edges, and thin tip fin leading edges; multiple measurements were made on a wide variety of unconventional control surfaces and appendages. Simultaneous measurements on the wide variety of surfaces required the selection of a sensor which was highly sensitive, small, and could be contoured to small local surface radii. The sensor chosen for these measurements was the Schmidt Boelter gage. The capability to calibrate Schmidt Boelter gages and compare a National Institute of Standards and Technology (NIST) traceable and certified standard is one reason this sensor was used for all of the measurements. Since each gage needs the measurement of two thermal parameters to obtain the required measurement parameter, the simultaneous measurement of 800 thermal parameters was required. The previous data acquisition system in these hypersonic wind tunnels at the AEDC was capable of measuring outputs for only 112 Schmidt Boelter gages simultaneously.

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Document Details

Document Type
Technical Report
Publication Date
Jan 14, 1999
Accession Number
ADA370988

Entities

People

  • C. T. Kidd
  • J. S. Carter
  • W. R. Hawkins

Organizations

  • American Institute of Aeronautics and Astronautics

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • C4I
  • Sensors

DTIC Thesaurus Topics

  • Accuracy
  • Acquisition
  • Aerodynamic Heating
  • Data Acquisition
  • Digital Data
  • Heat Flux
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hypersonic Wind Tunnels
  • Instrumentation
  • Leading Edges
  • Measurement
  • Surface Temperature
  • Test Facilities
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow