Further Investigations of Adaptive-Wall Wind Tunnels

Abstract

The objective of this investigation was to continue the assessment of the Calspan perforated-wall, segmented-plenum adaptive-wall wind tunnel for flows in which the tunnel walls are supercritical. An important aspect of the investigation was the development of a static-pipe measuring technique for determining the normal velocity distributions. This technique was developed to overcome the limitations on the number of flow-angle probe measurements that could be made in the Calspan tunnel. The flow about a static pipe in the presence of model/wall-induced disturbances was analyzed within the framework of slender-body theory to give the relationship between differential pressure measurements across the pipe and the steam-wise derivative of the normal velocity at the pipe centerline.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1980
Accession Number
ADA091774

Entities

People

  • C. E. Wittliff
  • D. C. Daughtry
  • J. C. Erickson Jr.

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Computational Fluid Dynamics
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Hydrodynamics
  • Instrumentation
  • Measurement
  • New York
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Swept Wings
  • Three Dimensional
  • Two Dimensional
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.