supercritical airfoil信息详情
超临界机翼;超临界翼形
The paper investigates the problem on vortex generator control boundary layer's separation of supercritical airfoil and wing for body configuration wing.───本文研究涡流发生器控制超临界翼型和翼身组合体机翼的附面层分离问题。
control of supercritical airfoil boundary layer separation is adapted using micro-vortex generators.───超临界翼型附面层分离控制适合采用微型涡流发生器。
drag values for a given airfoil(RAE2822 airfoil)were compared and discussed using the surface integration and wake integration methods under both subsonic and supercritical flow conditions.───在亚跨声速时分别采用了表面积分和尾迹积分求得给定翼型RAE2822的阻力。
This thesis investigated the effect of the airfoil modification on the aerodynamic performance of a certain supercritical airfoil.───鉴于此,本文选取某超临界翼型,探讨改型对超临界翼型气动性能的影响。
Investigation of boundary layer separation control for supercritical airfoil using micro vortex generator───微型涡流发生器控制超临界翼型边界层分离实验研究
Rapid Modeling of a Supercritical Airfoil's Integral Wing Plane Panels Based on Feature Mapping───基于特征映射的超临界机翼整体壁板板坯快速建模技术研究
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