NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Vortex flow aerodynamicsThe principal emphasis of the meeting was to be on the understanding and prediction of separation-induced vortex flows and their effects on vehicle performance, stability, control, and structural design loads. This report shows that a substantial amount of the papers covering this area were received from a wide range of countries, together with an attendance that was even more diverse. In itself, this testifies to the current interest in the subject and to the appropriateness of the Panel's choice of topic and approach. An attempt is made to summarize each paper delivered, and to relate the contributions made in the papers and in the discussions to some of the important aspects of vortex flow aerodynamics. This reveals significant progress and important clarifications, but also brings out remaining weaknesses in predictive capability and gaps in understanding. Where possible, conclusions are drawn and areas of continuing concern are identified.
Document ID
19920021703
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, J. H. B.
(Royal Aircraft Establishment Farnborough, United Kingdom)
Campbell, J. F.
(NASA Langley Research Center Hampton, VA., United States)
Young, A. D.
(Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine, France)
Date Acquired
August 15, 2013
Publication Date
April 1, 1992
Publication Information
ISBN: 92-835-0670-7
Subject Category
Aerodynamics
Report/Patent Number
AGARD-AR-299
Meeting Information
Meeting: Fluid Dynamics Panel Symposium
Location: Scheveningen
Country: The Netherlands
Start Date: October 1, 1990
End Date: October 4, 1990
Accession Number
92N30947
Distribution Limits
Public
Copyright
Other
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available