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Vortex Flow Aerodynamics [L'Aérodynamique des Ecoulements Tourbillonnaires]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. Topics of interest included vortex development and burst, modeling and validation of the full range of analytic methods, slender-body vortex flows at high angles of attack, vortex control and management, and unsteady vortex flow effects. In addition to the symposium papers, the results of the round table discussion are presented.
Document ID
19920003778
Acquisition Source
Legacy CDMS
Document Type
Other - AGARD Symposium - Conference Proceedings
Authors
Advisory Group for Aerospace Research and Development
(North Atlantic Treaty Organization Brussels, Belgium)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Publication Information
Publication: AGARD Conference Proceedings 494: Vortex Flow Aerodynamics
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0623-5
Subject Category
Aerodynamics
Report/Patent Number
AGARD-CP-494
AD-A244249
Meeting Information
Meeting: The Symposium of the Fluid Dynamics Panel
Location: Scheveningen
Country: NL
Start Date: October 1, 1990
End Date: October 4, 1990
Sponsors: North Atlantic Treaty Organization
Accession Number
92N12996
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
delta wings
computational fluid dynamics
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