Accession Number:

ADA244249

Title:

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

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1991-07-01

Pagination or Media Count:

534.0

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.

Descriptors:

• *SYMPOSIA
• FIGHTER AIRCRAFT
• PANELS
• BOUNDARY LAYER
• TURBULENT FLOW
• VORTICES
• FLOW VISUALIZATION
• AERODYNAMIC FORCES
• MANEUVERS
• FLOW
• FLIGHT ENVELOPE
• HIGH LIFT
• FLUID DYNAMICS
• WINGS
• SUPERSONIC CHARACTERISTICS
• FLOW SEPARATION
• AERODYNAMICS
• VORTEX GENERATORS
• THREE DIMENSIONAL FLOW

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE