Computational aerodynamic optimization of wing-design concept at supersonic conditions by means of the response surface method
作者: Mojtaba Dehghan ManshadiSoheil Aghajanian
作者单位: 1Department of Mechanical Engineering, Malek-Ashtar University of Technology
刊名: Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2018, Vol.40 (5), pp.1-15
来源数据库: Springer Journal
DOI: 10.1007/s40430-018-1150-4
关键词: Supersonic wingSweep angleComputational fluid dynamics (CFD)Response surface method (RSM)Aerodynamic shape optimization
英文摘要: Abstract(#br)In this paper, by means of computational fluid dynamics, a significant study has been made on the effects of geometric parameters of wing with capability of flying efficiently and cost-effectively at supersonic condition. Multi-objective optimization has been performed for the aerodynamic shape optimization of the wing configuration. The three-dimensional wing shape defined by four design variables is optimized. For achieving the most desirable aerodynamic efficiency (lift-to-drag ratio), Response Surface Method and Genetic Algorithm is utilized. To ensure the reliability of the solution and validating the numerical evaluation, flow around a delta wing is simulated and results are compared with credible numerical works. Furthermore, the particular design variables, which have...
全文获取路径: Springer  (合作)
分享到:

×