Conference Proceedings on Vortex Flow Aerodynamics Held in Scheveningen, The Netherlands on 1-4 October 1990

Abstract

The AGARD Fluid Dynamics Panel sponsored this Symposium to provide an update review of the aerodynamic effects of separation-induced vortex flows on the design and off-design performance of fighter aircraft. A better understanding is needed to predict and control these vortex flows throughout the flight envelope at subsonic, transonic, and supersonic speeds, and especially during high lift operations for take-offs, landings, and sustained and instantaneous maneuvers.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1991
Accession Number
ADA244249

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • High Lift Devices
  • Hydrodynamics
  • Mechanical Properties
  • Physics Laboratories
  • Standing Waves
  • Swept Wings
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aviation Science / Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics