NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Understanding the Flow Physics of Shock Boundary Layer Interactions Using CFD and Numerical AnalysesNo abstract available
Document ID
20150009937
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Friedlander, David
(NASA Glenn Research Center Cleveland, OH, United States)
Georgiadis, Nick
(NASA Glenn Research Center Cleveland, OH, United States)
Turner, Mark
(Cincinnati Univ. OH, United States)
Orkwis, Paul
(Cincinnati Univ. OH, United States)
Date Acquired
June 5, 2015
Publication Date
April 24, 2013
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
E-664422
Report Number: E-664422
Meeting Information
Meeting: Annual Shock Wave/Boundary Layer Interaction 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 475122.02.03.07.03
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available