Effects of Window Configuration on Model Pressure Distribution in Wind Tunnels with Perforated Walls

Abstract

Larger optical windows for access to the model flow field in the Arnold Engineering Development Center (AEDC) transonic wind tunnels will be required for optimum utilization of the laser velocimeter (LV). A combined analytical and experimental investigation was performed to assess the effects of such windows upon the performance of the perforated walls. The experimental results from the Aerodynamic Wind Tunnel (1T) indicate that although the wall interference characteristics of some window configurations approach the standard porous wall, none of the configurations tested exhibited adequate wave cancellation for all Mach numbers from M at infinity = 1.0 through 1.4. A variable porosity wall arrangement is described which appears to be capable of providing acceptable optical access without adversely affecting the tunnel flow field.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1981
Accession Number
ADA094213

Entities

People

  • F. L. Heltsley

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Bow Shock
  • Cancellation
  • Engineering
  • Flow
  • Flow Fields
  • Laser Velocimeters
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Standards
  • Transonic Wind Tunnels
  • United States
  • Velocimeters
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Directed Energy