Adding-Point Strategy for Reduced-Order Hypersonic Aerothermodynamics Modeling Based on Fuzzy Clustering

被引:5
作者
Chen Xin [1 ,2 ]
Liu Li [1 ,2 ]
Zhou Sida [1 ,2 ]
Yue Zhenjiang [1 ,2 ]
机构
[1] Beijing Inst Technol, Key Lab Dynam & Control Flight Vehicle, Minist Educ, Beijing 100081, Peoples R China
[2] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
基金
中国国家自然科学基金;
关键词
reduced order model; fuzzy clustering; hypersonic aerothermodynamics; adding-point strategy; RESPONSE-SURFACE METHOD; DESIGN; REDUCTION;
D O I
10.3901/CJME.2016.0128.016
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Reduced order models(ROMs) based on the snapshots on the CFD high-fidelity simulations have been paid great attention recently due to their capability of capturing the features of the complex geometries and flow configurations. To improve the efficiency and precision of the ROMs, it is indispensable to add extra sampling points to the initial snapshots, since the number of sampling points to achieve an adequately accurate ROM is generally unknown in prior, but a large number of initial sampling points reduces the parsimony of the ROMs. A fuzzy-clustering-based adding-point strategy is proposed and the fuzzy clustering acts an indicator of the region in which the precision of ROMs is relatively low. The proposed method is applied to construct the ROMs for the benchmark mathematical examples and a numerical example of hypersonic aerothermodynamics prediction for a typical control surface. The proposed method can achieve a 34.5% improvement on the efficiency than the estimated mean squared error prediction algorithm and shows same-level prediction accuracy.
引用
收藏
页码:983 / 991
页数:9
相关论文
共 27 条
[1]  
[Anonymous], 1963, J AEROSPACE ENG
[2]  
[Anonymous], 20060001 AIAA
[3]  
[Anonymous], 20102969 AIAA
[4]  
[Anonymous], PATTEN RECOGNITION F
[5]  
[Anonymous], 2008, 15 AIAA INT SPAC PLA
[6]  
[Anonymous], 20074263 AIAA
[7]  
[Anonymous], 20062960 AIAA
[8]  
[Anonymous], INT J NUMERICAL METH
[9]   Model Reduction of Computational Aerothermodynamics for Hypersonic Aerothermoelasticity [J].
Crowell, Andrew R. ;
McNamara, Jack J. .
AIAA JOURNAL, 2012, 50 (01) :74-84
[10]   Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow [J].
Culler, Adam J. ;
McNamara, Jack J. .
AIAA JOURNAL, 2010, 48 (08) :1721-1738