CFD Wing/Pylon/Finned Store Mutual Interference Wind Tunnel Experiment

Abstract

A wind tunnel test was conducted to obtain pressure and flow visualization data from geometrically simple wing and store shapes under mutual interference conditions with the store both at its carriage position and selected points along a realistic store separation trajectory. The test was conducted at nominal Mach numbers of 0.95 and 1.2 at a nominal Reynolds number of 2.4 million/ft. Data were acquired for wing and store angles of attack of 0, 2, and 6 deg.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1991
Accession Number
ADB152669

Entities

People

  • E. R. Heim

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • Computational Fluid Dynamics
  • Data Acquisition
  • Dynamic Pressure
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Mach Number
  • Measurement
  • Physical Properties
  • Plastic Explosives
  • Pressure Measurement
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.