Wind Tunnel Corrections for High Angle of Attack Models,

Abstract

This report contains papers on various wind tunnel correction methods used in high angles of attack tests. The paper were solicited from the various NATO countries and Canada, France, Germany, Netherlands, Sweden, United Kingdom and the United States. Several methods in use or under study are presented for closed, open and ventilated wind tunnels. The Mach number ranges up to the high subsonic and some methods are for are for incompressible flow. Techniques include vortex lattice, panel system of images, wall pressure and adaptive walls.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1981
Accession Number
ADA098058

Entities

People

  • M. L. Laster
  • R. O. Dietz

Organizations

  • AGARD

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • High Lift Devices
  • Hydrodynamics
  • Pressure Distribution
  • Pressure Measurement
  • Swept Wings
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Approximation Theory.
  • European Security and Defence Policy (ESDP).
  • Fluid Mechanics and Fluid Dynamics.