Reduction of Wall Interference Effects in the AEDC-PWT 1-FT Transonic Tunnel with Variable Perforated Walls

Abstract

An experimental investigation was conducted in the 1-ft transonic tunnel to assess the transonic wave cancellation performance of six variable porosity, test section wall designs. The wall interference effects were detected utilizing a 20-deg cone-cylinder static pressure model of 1-percent blockage. The variable wall porosity designs incorporated a sliding cutoff plate with hole geometry identical to a fixed airside plate. Upstream movement of the sliding plates for decreasing porosity provided a test section boundary which successfully eliminated wave reflection wall interference throughout most of the transonic range.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1969
Accession Number
AD0851575

Entities

People

  • J. L. Jacocks

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Engineering
  • Geometry
  • Government Procurement
  • Governments
  • Instrumentation
  • Mach Number
  • Nomenclature
  • Porosity
  • Pressure Distribution
  • Static Pressure
  • Tennessee
  • Three Dimensional
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.