Conceptual design of cruise missile based on technology of modern design of experiment

[1] 王振国,陈小前,罗文采,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社,2006:110 Wang Zhenguo,Chen Xiaoqian, Luo Wencai, et al. Research on the theory and application of multidisciplinary design optimization of flight vehicles [M]. Beijing: National Defense Industry Press, 2006:110(in Chinese) [2] Fang K T, Ma C. Wrap-around L2-discrepancy of random sampling,latin hypercube and uniform designs [J]. Journal of Complexity, 2001,17:608-624 [3] Knill D L, Giunta A A, Baker C A,et al. Response surface models combining linear and Euler aerodynamics for supersonic transport design [J]. Journal of Aircraft, 1999, 36(1):75-86 [4] Auzins J. Direct optimization of experimental designs //10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. New York: , 2004 [5] Giunta A A Steven F, Wojtkiewicz Jr, et al. Overview of modern design of experiments methods for computational simulation //41st Aerospace Sciences Meeting and Exhibit. Reno, Nevada: , 2003 [6] Mateen-ud-Din Q. Multi-disciplinary analysis and design using intelligent and non-deterministic approaches for the conceptual design of space launch vehilcle .Beijing:School of Astronautics, Beijing University of Aeronautics and Astronautics, 2006 [7] He Linshu. Solid ballistic missiles design[M]. Beijing:Beijing University of Aeronautics and Astronautics Press, 2004:47-50