National Research Council. High speed research aeronautics and space engineering board U.S. supersonic commercial aircraft: assessing NASA’s high speed research program[M]. Washington, D.C.: National Academy Press, 1997.
[2]
Seebass A R. Sonic boom theory[J]. Journal of Aircraft, 1969, 6(13): 177-184.
[3]
Haas A, Kroo I. A multi-shock inverse design method for low-boom supersonic aircraft[R]. AIAA - 2010-843, 2010.
[4]
Li W, Shields E, Le D. Interactive Inverse Design Optimization of Fuselage Shape for Low-Boom Supersonic Concepts[J]. Journal of Aircraft, 2008,45(4):1381–1398.
[5]
Howe D C. Improved sonic boom minimization with extendable nose spike[R]. AIAA-2005-1014, 2005.
[6]
Donald Freund, Frank Simmons. Quiet spike? prototype flight test results[R].AIAA-2007-1778,2007.
[7]
陈鹏,李晓东.基于Khokhlov-Zabolotskaya-Kuznetsov方程的声爆频域预测法[J].航空动力学报,2010,25(2):359-365. (Chen Peng. 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))
[8]
但聃.基于声爆和起降噪声要求的超音速公务机设计[D].硕士学位论文,中国航空研究院611所,2010:31-35.(Dan Dan. Supersonic business design based on request of sonic boom and takeoff/approaching acoustics[D].Chengdu Aircraft Research and Design Institute,2010.(in chinese) )
[9]
冯晓强,李占科,宋笔锋. 超音速客机音爆问题初步研究[J]. 飞行力学, 2010, 28(6): 21-27. (Feng Xiaoqiang, Li Zhanke, Song Bifeng. Preliminary analysis on the sonic boom of supersonic aircraft[J]. Flight Dynamics,2010,28(6):21-27(in Chinese))
[10]
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[J].航空学报,2011,32(11):1980-1986. (Feng Xiaoqiang, Li Zhanke, Song Bifeng. A research on inverse design method of a lower sonic boom supersonic aircraft configuration[J]. Acta Aeronautica et Astronautica sinica,2011,32(11):1980-1986(in chinese))
[11]
冯晓强. 声爆计算方法研究及在超声速客机设计的应用[D].硕士学位论文,西北工业大学,2012:43-53.(Feng Xiaoqiang. The research of sonic boom prediction method and application in supersonic aircraft design[D]. Northwestern Polytechnical university,2012.(in chinese))
[12]
Isik Ali Ozcer. Sonic boom prediction using euler / full potential methodology[R].AIAA-2007-0369,2007.
[13]
Carlson H W. A wind tunnel investigation of the effect of body shape on sonic boom pressure distributions[R]. NASA TND-3106, 1965.
[14]
Thomas C L. Extrapolation of sonic boom pressure signatures by the waveform parameter method[R]. NASA TND-6832, 1972.
[15]
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.
[16]
J D Anderson. Fundamentals of aerodynamics[M].New York,McGraw-Hill companies,2005.