Ogawa, H and Babinsky, H (2008) Shock/boundary-layer interaction control using three-dimensional bumps in supersonic engine inlets. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, 7-1-2008 to 10-1-2008, Reno, Nevada, USA.
Full text not available from this repository.
|Item Type: ||Conference or Workshop Item (UNSPECIFIED)|
|Additional Information: ||Event type = conference AIAA-2008-0599 This paper could not be found on Zetoc. Conference Proceedings have been published.CB(14.01.09)|
|Divisions: ||Div A > Fluid Mechanics|
|Depositing User: ||Cron Job|
|Date Deposited: ||28 Oct 2011 17:05|
|Last Modified: ||13 Jan 2014 01:22|
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