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오일러 방정식과 자유 후류법을 이용한 헬리콥터 로터의 비정상 공력 해석 연구
이재훈(Jaehun Lee),위성용(Seongyong Wie),권장혁(JangHyuk Kwon),이덕주(Duckjoo Lee),김대희(Dahee Kim) 한국전산유체공학회 2007 한국전산유체공학회 학술대회논문집 Vol.2007 No.-
In this study the unsteady aerodynamic analysis of a hovering helicopter rotor is performed For the accurate flow field analysis Euler equations and the free wake method are coupled The Euler equations are solved to find the pressure distribution around the rotor, and free wake method is used to give the boundary condition for the solution of Euler equations. Also, vortex strength and wake motion after the rotor are simulated by the free wake method The accuracy of the present method is compared with the source sink model. The present method is applied to the hovering Caradonna-Tung rotor and compared with experimental results.