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Effect of Hybrid Flow Control on a Normal Shock Boundary-Layer InteractionNo abstract available
Document ID
20150009935
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Hirt, Stefanie
(NASA Glenn Research Center Cleveland, OH, United States)
Vyas, Manan
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 5, 2015
Publication Date
April 24, 2013
Subject Category
Aerodynamics
Report/Patent Number
E-664420
Meeting Information
Meeting: Shock Wave/Boundary-Layer Interraction Workshop (SWBLI)
Location: Dayton, OH
Country: United States
Start Date: April 24, 2013
End Date: April 25, 2013
Sponsors: NASA Headquarters
Funding Number(s)
WBS: WBS 794072.02.03.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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