| Citation: | Liu Hang, Zhu Ziqiang, Fu Hongyan, et al. Comparison between adaptive and biobjective optimization wing's aerodynamic features[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 461-465. (in Chinese)
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[1] Richardson D. Stealth warplanes[M]. London:Salamander Book,1989 [2]Bushgens G S. Aerodynamics, stability and controllability of supersonic aircraft [M]. Moscow:Navka Fizmatlit, 1998. 224~230 [3] 刘 航,朱自强,吁日新,等.自适应翼型的气动外形优化设计[J].航空学报, 2002, 23(4):289~293 Liu Hang,Zhu Ziqiang, Yu Rixin, et al. Optimization design of adaptive airfoils aerodynamics shape [J]. Acta Aeronautica Et Astronautica Sinica, 2002,23 (4):289~293(in Chinese) [4] Powell M J D. An efficient method for inding the minimum of a function of several variables without calculation derivatives[J]. Computer Journal, 1964, 7(2):155~162 [5]Li J, Zhu Z Q,Chen H M, et al. The Euler and Navier-Stokes solutions of a 3-D wing with aileron[J]. Acta Mechanica, 1999,138:51~59 [6] 吁日新,朱自强.双目标/双学科数值优化计算[J].航空学报,2002,23(4):330~333 Yu Rixin Zhu Ziqiang. Computation of the biobjective/bidisciplinary numerical optimization[J]. Acta Aeronautica Et Astronautica Sinica.2002,23 (4):330~333(in Chinese)
|
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Liu Hang, Zhu Ziqiang, Fu Hongyan, et al. Comparison between adaptive and biobjective optimization wing's aerodynamic features[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 461-465. (in Chinese)
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