[1]
Jiguang Hao, Yi Jiang, and Qi Liu. Numerical simulation on aerodynamic heating process of certain missile's head using a method of fluid-solid coupled. Journal of Projectiles, Rockets, Missiles and Guidance, 2006, 26(4): 230-232. (In Chinese)
Google Scholar
[2]
Eric L. Blades, and James C. Newman. Computational aeroelastic analysis of an unmanned aerial vehicle using U2NCLE. AIAA Paper 2007-2237.
DOI: 10.2514/6.2007-2237
Google Scholar
[3]
Gang Xia, Xinjian Liu, Wenke Cheng, and Zizeng Qin. Numerical simulation of coupled aeroheating and solid heat penereation for a hypersonic blunt body. Journal of National University of Defense Technology, 2003, 25(1): 35-41. (In Chinese)
Google Scholar
[4]
Xiangren Geng, Hanxin Zhang, Qin Shen, and Shuchun Gao, Study on an integrated algorithm for the flowfields of high speed vehicles and the heat transfer in solid structures. Acta Aerodynamic Sinica, 2002, 20(4): 422-427. (In Chinese)
Google Scholar
[5]
Joris Degroote, Antonio Souto-Iglesias, Wim Van Paepegem, et al. Partitioned simulation of the interaction between an elastic structure and free surface flow. Computer Methods in Applied Mechanics and Engineering, 2010, 199: 2085-2098.
DOI: 10.1016/j.cma.2010.02.019
Google Scholar
[6]
Juan R.Cebral, and Rainald L. On the loose coupling of implicit time-marching codes. AIAA Paper 2005-1093.
DOI: 10.2514/6.2005-1093
Google Scholar
[7]
Rainald L., Chi Yang, Juan Cebral, et al. Fluid-structure-thermal interaction using a loose coupling algorithm and adaptive unstructured grids. AIAA Paper 98-2419.
DOI: 10.2514/6.1998-2419
Google Scholar
[8]
Charbel Farhat, and Charbel Lesoonne. A conservative algorithm for exchanging aerodynamic and elastodynamic data in aeroelastic. AIAA Paper 98-0515.
DOI: 10.2514/6.1998-515
Google Scholar
[9]
Juan Raul Cebral, and Ranald L. Conservative load projection and tracking for fluid-structure problems. AIAA Paper 96-0797.
Google Scholar
[10]
Vipperla B. Venkayya, and Victoria A, Tischler. Force and displacement transformations for aero-structure interaction analysis. AIAA Paper 2004-4328.
DOI: 10.2514/6.2004-4328
Google Scholar
[11]
Sadeghi M., and Liu F. Application of three-dimensional interfaces for data transfer in aeroelastic computations. AIAA Paper 2004-5376.
Google Scholar
[12]
Aukje De Boer, Hester Bijl, and Alexander Van Zuijlen. Comparing different methods for the coupling of non-matching meshes in fluid-structure interaction computations. AIAA Paper 2005-4620.
DOI: 10.2514/6.2005-4620
Google Scholar
[13]
Shaoyun Song, and Shiqi Li. Mixed method of node load interpolation in collaborative simulation of coupled problem. Computer Simulation, 2006, 23(8): 73-75. (In Chinese)
Google Scholar
[14]
Lizhou Li, Jingchao Wang, Zhenzhou Lu, and Zhufeng Yue. A load interpolation transfer method among disciplines in parametric space. Journal of Aerospace Power, 2007, 22(7): 1050-1054. (In Chinese)
Google Scholar
[15]
Xiaomin An , Min Xu , and Shilu Chen. A new interface mapping and marching method for aeroelasticity. Journal of Astronautics, 2008, 29(5): 1473-1476. (In Chinese)
Google Scholar
[16]
Allen C.B., and Rendall T.C.S. Unified approach to CFD-CSD interpolation and mesh motion using radial basis functions. AIAA Paper 2007-3804.
DOI: 10.2514/6.2007-3804
Google Scholar
[17]
Duchon J. Splines minimizing rotation-invariant semi-norms in sobolev spaces. Constructive Theory of Functions of Several Variables, 1976: 85-100.
DOI: 10.1007/bfb0086566
Google Scholar
[18]
Chen P. C., and Jadic I. Interfacing of fluid and structural models via innovative structural boundary element method. AIAA Journal, 1998, 36(2) 282-287.
DOI: 10.2514/3.13810
Google Scholar
[19]
Min Xu, Shilu Chen. Study of date exchange metod for coupling computational CFD/CSD. Chinese Journal of Applied Mechanics, 2003,21(2) 33-37.
Google Scholar