BALANCE FOR MEASURING SKIN FRICTION IN THE PRESENCE OF HEAT TRANSFER

Abstract

The development of a skin-friction balance to be used in a wind tunnel with heat-transfer conditions is described. The balance is a null-type device with a floating head element whose temperature can be maintained between 100K and 345K. This is accomplished with a cooled or heated jacket that is placed in direct contact with the friction element. At the desired element temperature the jacket is separated from the element and the shear-force data is taken. The balance was used in a Mach 5 supersonic flow with moderate heat- transfer rates. Shear forces ranging from 0.05 gm/sq cm to 1 gm/sq cm have been measured and higher ranges can be obtained by simply changing a coil spring.

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Document Details

Document Type
Technical Report
Publication Date
Jun 10, 1969
Accession Number
AD0697648

Entities

People

  • Donald B. Risher
  • James R. Bruno
  • William J. Yanta

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Barometric Pressure
  • Boundaries
  • Boundary Layer
  • Calibration
  • Flow
  • Fluid Mechanics
  • Heat Transfer
  • Instrumentation
  • Layers
  • Measurement
  • Mechanics
  • Modulus Of Elasticity
  • Munitions
  • Ordnance Laboratories
  • Pressure Gradients
  • Skin Friction
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Structural Dynamics.
  • Thermal Physics or Thermal Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow