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Measurements on wing-tip blowingThe aerodynamics of a rectangular wing with a jet exhausting in the spanwise direction from the tips has been explored experimentally. By effectively changing the span of the wing as well as outwardly displacing the tip vortices, such jets can induce aerodynamic forces that could be used for roll and lateral control of aircraft. The concept has been investigated for a variety of jet intensities, angles of attack, and aspect ratios. The results appear to confirm theoretically predicted scaling laws for lift gain and moment generation due to blowing.
Document ID
19860019450
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tavella, D.
(Stanford Univ. CA, United States)
Wood, N.
(Stanford Univ. CA, United States)
Harrits, P.
(Stanford Univ. CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
JIAA-TR-64
NASA-CR-176930
NAS 1.26:176930
Report Number: JIAA-TR-64
Report Number: NASA-CR-176930
Report Number: NAS 1.26:176930
Accession Number
86N28922
Funding Number(s)
CONTRACT_GRANT: NCC2-271
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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