⑥跨声速轴流压气机转子NASA(National Aeronautics and Space Administration) Rotor 37三维黏性绕流;⑦跨声速风扇转子NASA Rotor 67三维黏性绕流)算例表明:该方法的计算效率比传统的WENO格式有较大的提高
大部分典型算例能够提高3~5倍
而且可以获取复杂流场中高分辨率的激波结构以及涡系分布
可以得到与有关实验数据较为吻合的数值结果.
Abstract
Three-dimensional and two-dimensional wavelet sigularity analysis was introduced in complicated flow and a high-order
high-resolution numerical method was developed.The core of this new method is the analysis of Hlder exponent α of complicated flow.The Hlder exponent α depends on wavelet transform and multi-dimensional wavelet analysis.In order to complete the multi-resolution analysis in two-dimensional and three-dimensional Euclidean space
scale basis and wavelet basis have been introduced in scale space and wavelet space.For two-dimensional and three-dimensional cases
scale basis and wavelet basis were constructed by one scale function and by three wavelet functions and seven wavelet functions respectively.High-resolution
high-order WENO (weighted essential non-oscillatory) scheme and high-order central difference scheme can be chosen adaptively according to the results of wavelet sigularity analysis.A series of examples in two-dimensional ( (1) forward facing step problem
(2) double Mach reflection of a strong shock problem
(3) two-dimensional Riemann problem
(4) two-dimensional transonic flow past RAE2822 airfoil problem
NASA (National Aeronautics and Space Administration) Rotor 37 three-dimensional viscous flow and (7) NASA Rotor 67 three-dimensional viscous flow) were computed.The computation results have been compared with the experiment results in related references and showed that this new numerical method can not only improve the computation efficiency significantly(the efficiency can be increased by 3~5 times for most examples)
but also capture the shock with high-resolution and vortices with an acceptable order.