Experimental investigation of aerodynamics performance of multielement airfoil with leadingedge slat.
带缝翼多段翼型气动特性的实验研究
An Experimental Study on Location of Transitional Separation Bubble on a Low Reynolds Numbers Airfoil.
确定低雷诺数翼型转捩分离泡位置的实验研究
A hinged vertical airfoil mounted at the tail of an aircraft and used to make horizontal course changes.
安装在飞机尾部的用来改变水平方向的垂直机翼。
The Web version the code allows for the prescription the inviscid velocity distribution about the airfoil.
网上版得代码允许处方粘速度分布得翼型。
The mathematical transformation is fixed and the airfoil is moved to generate different airfoil geometries.
数学变换是固定机翼得翼型几何移到产生不同。
Airfoil trailingedge vortex separation occurs, resulting in movement of the flow field near the airfoil stall.
翼型后缘出现的分离涡, 导致翼型附近流场的流动失速。
Inconel alloy spindlevane with trenching machined into the airfoil surface to allow for instrumentation wiring.
因科镍合金叶片安装到翼型表面，以便仪器接线。
In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology.
基于响应面方法进行了跨声速翼型的气动优化设计。
Numerical research of the influence of airfoil stall and Reynolds number change on wind turbine aerodynamic performance
翼型失速及雷诺数变化对风力机气动性能影响的数值研究
The afterbody form finalizing sheet is in an arc shape， the tail part raises upwards to assist the airfoil to be the arc.
机尾定型片呈弧形，其尾部上翘，辅助机翼成弧形。
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