Showing results 4 to 8 of 8
Numerical investigation of effect of crossflow transition on rotor blade performance in hover Han, Jaeseong; Hwang, Je Young; Kwon, Oh Joon, AEROSPACE SCIENCE AND TECHNOLOGY, v.114, 2021-07 |
Numerical Study of Aerodynamic Performance of a Multirotor Unmanned-Aerial-Vehicle Configuration Hwang, Je Young; Jung, Min Kyu; Kwon, Oh-Joon, JOURNAL OF AIRCRAFT, v.52, no.3, pp.839 - 846, 2015-05 |
Numerical Study of Free-Flight Projectiles Air-Launched from a Rotorcraft Jo, Sung Min; Hwang, Je Young; Kwon, Oh Joon, 7th Asian/Australian Rotorcraft Forum, The Korean Society For Aeronautical And Space Sciences, 2018-10-30 |
Numerical Study of PSP Rotor Blades Using a γ-Reθt-CF+ Turbulent Transition Model Hwang, Je Young; Kwon, Oh Joon, AIAA SciTech, AIAA SciTech, 2019-01-08 |
비정렬 혼합 격자계 유동 해석자를 이용한 헬리콥터 블레이드에 대한 수치적 연구 = Numerical investigation of helicopter blades by using an unstructured mixed mesh flow solverlink 황제영; 권오준; et al, 한국과학기술원, 2019 |
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