Evaluation on Interference Effects on a Lifting Model in the AEDC-PWT 4- Ft Transonic Tunnel

Abstract

Tests were conducted to evaluate subsonic and supersonic wall interference effects and general data quality using a modified F-111A aircraft model of 0.6-percent blockage. The tunnel is equipped with inclined-hole, variable porosity test section walls.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1970
Accession Number
AD0868290

Entities

People

  • J. L. Jacocks

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Agreements
  • Air Force
  • Aircraft Models
  • Boundary Layer
  • Data Reduction
  • Engineering
  • Flags
  • Flow Visualization
  • Horizontal Stabilizers
  • Instrumentation
  • Mach Number
  • Measurement
  • Models
  • Pressure Distribution
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow