한국전산유체공학회:학술대회논문집
- 2010.05a
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- Pages.37-39
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- 2010
DYNAMIC STALL ANALYSYS OF A MID-SIZED AIRCRAFT
중형항공기 동적 실속 특성 해석
- Published : 2010.05.13
Abstract
Aerodynamic analysis was done for a fuselage and wing configuration of a mid-sized aircraft using 3-dimensional Navier-Stokes solver. Various turbulent models including a transitional SST were implemented to observe a dynamic stall as well as cruise characteristics. Also, different mesh moving methods were evaluated. Flow hysteresis which causes dynamic stall was investigated through flow field investigations.
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