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The Effect of Tabs on a Jet in a Cross-FlowA tab placed on the leeward side of the nozzle was expected to increase jet penetration into the cross-flow. An experiment at UTRC showed insignificant effect. The primary objective of the present study was to confirm and explain the ineffectiveness. The overall approach of the study was to conduct experiments in a low-speed wind tunnel and to conduct hot-wire measurements for mean velocity and streamwise vorticity fields.
Document ID
19980013186
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Khairul Bmq Zaman (Lewis Research Center Cleveland, Ohio, United States)
Judith Foss Van Zante (Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 17, 2013
Publication Date
December 12, 1996
Publication Information
Publication: Conference Publication 1996 Coolant Flow Management Workshop
Publisher: National Aeronautics and Space Administration
Volume: NASA-CP-10195
Issue Publication Date: January 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: 1996 Coolant Flow Management Workshop
Location: Cleveland, OH
Country: US
Start Date: December 12, 1996
End Date: December 13, 1996
Sponsors: Ohio Aerospace Institute
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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