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Control of separated flow past a cylinder using tangential wall jet blowingA theoretical analysis is conducted to study the effect of a tangential wall jet on the control of two dimensional separated flow past a circular cylinder. For a tangential wall jet, the mathematical model derived previously is used and the vortex cloud method is adopted for the calculation of the external flow field. For certain limiting cases, the governing equations are simplified and closed forms of solutions for the wall jet parameters can be obtained. It is observed that the wall jet is very efficient in reducing drag by delaying the separation point in the range of small blowing strength. The suction force induced by the wall jet is negligible to the drag due to the external stream. However this suction increases the drag when the blowing strength is large.
Document ID
19890019955
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Oh, Sejong
(Stanford Univ. CA, United States)
Roberts, Leonard
(Stanford Univ. CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:185918
NASA-CR-185918
JIAA-TR-93
Report Number: NAS 1.26:185918
Report Number: NASA-CR-185918
Report Number: JIAA-TR-93
Accession Number
89N29326
Funding Number(s)
CONTRACT_GRANT: NCC2-55
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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