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Numerical simulation of wing lift augmentation with spanwise tip blowingNavier-Stokes simulations are used to study the phenomena of wing lift augmentation with spanwise tip blowing. Flowfields calculated for varying blowing conditions are analyzed to determine the mechanisms responsible for providing lift augmentation. It is found that both viscous and inviscid effects are important.
Document ID
19880035065
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Caruso, S. C. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Mendenhall, M. R. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Childs, R. E. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 88-0396
Report Number: AIAA PAPER 88-0396
Accession Number
88A22292
Funding Number(s)
CONTRACT_GRANT: F33615-83-C-3033
Distribution Limits
Public
Copyright
Other

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