한국전산유체공학회:학술대회논문집
- 한국전산유체공학회 2007년도 춘계 학술대회논문집
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- Pages.45-49
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- 2007
초음속 고받음각 유동을 위한 난류 모델 비교 연구
COMPARATIVE STUDY ON TURBULENCE MODELS FOR SUPERSONIC FLOW AT HIGH ANGLE OF ATTACK
초록
Asymmetric force and vibration caused by separation flow at high angle of attack affect the stability of supersonic missile. As a preliminary study we verified the effect of turbulence model through general 3-D slender body for the supersonic flow at high angle of attack.