| [1] Menexiadis G. Long-range propagation of sonic boom form the concorde airliner: analyses and simulations. Journal of Aircraft, 2008, 45(5): 1612-1618.[2] Seebass A R. Sonic boom theory. Journal of Aircraft, 1969, 6(13): 177-184.[3] Kusunose K. A fundamental study for the development of boomless supersonic transport aircraft. AIAA-2006- 654, 2006.[4] Li W, Shields E, Le D. Interactive inverse design optimization of fuselage shape for low-boom supersonic concepts. Journal of Aircraft, 2008, 45(4): 1381-1398.[5] Howe D C. Development of the Gulfstream quiet spike for sonic boom minimization. AIAA-2008-124, 2008.[6] Knight M. Quiet spike prototype morphing performance during flight test. AIAA-2008-127, 2008.[7] Zi Z H, Lv Y L. Study of passive acoustic locating of supersonic multi-target. Computer Engineering and Applications, 2010, 46(10): 202-205. (in Chinese) 字正华, 吕永林.多超声速目标被动声定位技术研究.计算机工程与应用, 2010, 46(10): 202-205.[8] Chen P, Li X D. Frequency domain method for predicting sonic boom propagation based on Khokhlov-Zabolotskaya-Kuznetsov equation. Journal of Aerospace Power, 2010, 25(2): 359-365.(in Chinese) 陈鹏,李晓东.基于Khokhlov-Zabolotskaya-Kuznetsov方程的声爆频域预测. 航空动力学报, 2010, 25(2): 359-365.[9] Dan D. Supersonic business design based on request of sonic boom and takeoff/approaching acoustics. Chengdu: Chengdu Aircraft Research and Design Institute, 2010.(in Chinese) 但聃. 基于声爆和起降噪声要求的超音速公务机设计. 成都: 成都飞机设计研究所, 2010.[10] Feng X Q, Li Z K, Song B F. Preliminary analysis on the sonic boom of supersonic aircraft. Flight Dynamics, 2010, 28(6): 21-27.(in Chinese) 冯晓强, 李占科, 宋笔锋. 超音速客机音爆问题初步研究. 飞行力学, 2010, 28(6): 21-27.[11] Feng X Q, Li Z K, Song B F. A research on inverse design method of a lower sonic boom supersonic aircraft configuration. Acta Aeronautica et Astronautica Sinica, 2011, 32(11): 1980-1986.(in Chinese) 冯晓强, 李占科, 宋笔锋.超声速客机低音爆布局反设计技术研究. 航空学报, 2011, 32(11): 1980-1986.[12] Feng X Q. The research of sonic boom prediction method and application in supersonic aircraft design. Xi'an: School of Aeronautics, Northwestern Polytechnical University, 2012.(in Chinese) 冯晓强. 声爆计算方法研究及在超声速客机设计的应用. 西安: 西北工业大学航空学院, 2012.[13] Rallabhandi S. Sonic boom minimization through vehicle shape optimization and probabilistic acoustic propagation.Georgia Institute of Technology, 2005.[14] Liang Y, Cheng X Q, Li Z N. Multi-object aerodynamic configuration parameter design using kriging approximation. Acta Aeronautica et Astronautica Sinica, 2010, 31(6): 1141-1148.(in Chinese) 梁煜, 程小全, 郦正能. 基于代理模型的气动外形平面参数多目标匹配设计.航空学报, 2010, 31(6): 1141-1148.[15] Kalyanmoy D, Pratap A. A fast and elitist multi-objective genetic algorithm: NSGA-Ⅱ. IEEE Transactions on Evolutionary Computation, 2002, 6(2): 182-197.[16] Plotkin K J. State of the art of sonic boom modeling. Journal of Acoustical Society of America, 2002, 111(1): 530-536.[17] Siclari M, Darden C. A euler code prediction of near to mid-field sonic boom pressure signature. AIAA-1990-4000, 1990.[18] Thomas C L. Extrapolation of sonic boom pressure signatures by the waveform parameter method. NASA TND-6832, 1972.[19] Page J A. An efficient method for incorporating computational fluid dynamics into sonic boom prediction.AIAA-1991-53882, 1991.as C L. Extrapolation of sonic boom pressure signatures by the waveform parameter method[R]. NASA TND-6832, 1972.[18] J.A.Page. An efficient method for incorporating computational fluid dynamics into sonic boom prediction[R].AIAA-1991-53882,1991.[19] Stevens.S.S. Perceived level of noise by Mark VII and decibels. The Journal of the Acoustical Society of America,1972;51(2):575-601. |
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