한국전산유체공학회:학술대회논문집
- 2008.08a
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- Pages.73.1-73.1
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- 2008
VORTEX BREAKDOWN DUE TO FLAPS ON A 60$^{\circ}$ DELTA WING- BODY
- Gopinath, N. (National Trisonic Aerodynamic Facilities National Aerospace Laboratories) ;
- Sridharan, R. (National Trisonic Aerodynamic Facilities National Aerospace Laboratories)
- Published : 2008.08.17
Abstract
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