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) |
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| 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) |
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| Subjects: | UNSPECIFIED |
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| Divisions: | Div A > Fluid Mechanics |
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| Depositing User: | Cron Job |
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| Date Deposited: | 28 Oct 2011 17:05 |
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| Last Modified: | 15 Nov 2011 10:27 |
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| DOI: | |
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