1. In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM). 基于响应面方法进行了跨声速翼型的气动优化设计。
2. In this paper, the optimization design of the transonic wing at single and multiple design-points is performed by RSM. 本文将响应面法引入到气动数值优化设计中,完成了跨声速机翼单、多目标多约束气动优化设计。
3. Computational Fluid Dynamics (CFD) and optimization technique are combined in this paper for the purpose of optimal aerodynamic design of transonic airfoil. 将计算流体动力学(CFD)与最优化技术相结合,通过数值求解欧拉方程,对翼型绕流流场作出了数值模拟。
英英解释
adj.
1. (of speed) having or caused by speed approximately equal to that of sound in air at sea level