Heat-Transfer Measurements on a 5-Deg Sharp Cone Using Infrared Scanning and On-Board Discrete Sensor Techniques

Abstract

Heat transfer data were obtained in hypersonic flow on a slender 5- deg half angle cone to evaluate the accuracy and test procedure of an infrared thermal mapping technique. Data were also obtained using discrete on board meansurements for comparative purposes.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1978
Accession Number
ADA070363

Entities

People

  • D. E. Boylan
  • J. A. Noble

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Data Reduction
  • Equations
  • Flow
  • Free Stream
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hypersonic Flow
  • Hypersonic Wind Tunnels
  • Infrared Scanning
  • Instrumentation
  • Mach Number
  • Measurement
  • Surface Temperature
  • Test Facilities
  • Wind Tunnels

Readers

  • Fluid Dynamics.
  • Sensor Fusion and Tracking Systems.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow