Time-Adaptive, Loosely Coupled Strategy for Conjugate Heat Transfer Problems in Hypersonic Flows

被引:55
作者
Zhang, Shengtao [1 ]
Chen, Fang [1 ]
Liu, Hong [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
MULTIDIMENSIONAL COMPRESSIBLE FLOWS; CONTROL-THEORETIC TECHNIQUES; MONOTONIC NUMERICAL-METHODS; RUNGE-KUTTA METHODS; STEPSIZE SELECTION; THERMAL-ANALYSIS; LIMITING PROCESS; ACCURATE; EQUATIONS; EFFICIENT;
D O I
10.2514/1.T4278
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper describes the development of a novel, time-adaptive, loosely coupled analysis strategy for efficiently predicting the conjugate heat transfer problems in hypersonic flows. Considering manyorders of magnitude disparity of physical characteristic time scales between hypersonic flow behavior and structural heat transfer, a loosely coupled strategy is first developed to efficiently couple an aerodynamic flow computational fluid dynamics solver with a structural heat transfer finite element method solver. Then, an adaptive coupling time stepsize approach based on a control theory point of view is proposed and embedded into this strategy for further efficiency. Finally, the performance of the proposed time-adaptive, loosely coupled analysis strategy is evaluated by performing conjugate heat transfer simulations over a cylindrical leading-edge model. The computational results are presented and analyzed, indicating that this strategy can offer the potential for significant improvements in predicting the long-duration conjugate heat transfer problems in hypersonic flows in terms of efficiency and/or accuracy.
引用
收藏
页码:635 / 646
页数:12
相关论文
共 37 条
[1]  
*ANSYS INC, 2011, ANSYS MECHANICAL APD
[2]  
*ATL STEELS AUSTR, STAINLESS STEEL GRAD
[3]   Critical hypersonic aerothermodynamic phenomena [J].
Bertin, JJ ;
Cummings, RM .
ANNUAL REVIEW OF FLUID MECHANICS, 2006, 38 :129-157
[4]   SHOCK-WAVE SHAPES AROUND SPHERICAL-AND CYLINDRRICAL-NOSED BODIES [J].
BILLIG, FS .
JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (06) :822-&
[5]   A time-adaptive fluid-structure interaction method for thermal coupling [J].
Birken, Philipp ;
Quint, Karsten J. ;
Hartmann, Stefan ;
Meister, Andreas .
COMPUTING AND VISUALIZATION IN SCIENCE, 2010, 13 (07) :331-340
[6]   FLOW-THERMAL-STRUCTURAL STUDY OF AERODYNAMICALLY HEATED LEADING EDGES [J].
DECHAUMPHAI, P ;
THORNTON, EA ;
WIETING, AR .
JOURNAL OF SPACECRAFT AND ROCKETS, 1989, 26 (04) :201-209
[7]   THEORY OF STAGNATION POINT HEAT TRANSFER IN DISSOCIATED AIR [J].
FAY, JA ;
RIDDELL, FR .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (02) :73-&
[8]  
FERRERO P, 2008, AIAA PAPER 2008 4247
[9]  
Giles MB, 1997, INT J NUMER METH FL, V25, P421, DOI 10.1002/(SICI)1097-0363(19970830)25:4<421::AID-FLD557>3.0.CO
[10]  
2-J