摘要
从某型高空长航时概念验证机的总体分析出发，采用数值计算与数理统计相结合的二次响应面方法，以翼型的最大巡航效率为设计目标，发展了一种适合于工程实际应用的翼型优化设计方法。
In this paper, following the overall design of a High -Altitude Long- Endurance concept UAV , Using CFD numerical calculation and statistics method, aerodynamic optimization design technology based on Response Surface Methodology（RSM） is developed. The design object is to achieve highest cruising efficiency. This method is effective and will be very attractive for practical use.
出处
《电光系统》
2008年第2期28-30,23,共4页
Electronic and Electro-optical Systems
关键词
雷诺数
翼型
响应面
优化设计
Renault number
Airfoil profile
RSM
Optimization design
