冯顺山,完颜振海.平头弹超音速尾流对飘带伞气动特性的影响[J].北京理工大学学报,2011,31(6):643-646. Feng Shunshan,Wanyan Zhenhai. Influence of flat-faced submunition\'s supersonic wake flow on the aerodynamic characteristics of disk-streamer parachute[J]. Transactions of Beijing Institute of Technology,2011,31(6):643-646. (in Chinese)
[2]
回返技术翻译组.气动力减速器原理及设计[M].北京:国防工业出版社, 1976. Translation Group of Inversion Technology. Mechanism and design of aerodynamic decelerator[M]. Beijing: National Defense Industry Press, 1976. (in Chinese)
[3]
完颜振海,冯顺山,董永香,等.超音速伞弹流场特性数值分析[J].兵工学报,2011,32(5):520-525. Wanyan Zhenhai,Feng Shunshan,Dong Yongxiang,et al. Numerical analysis of flow characteristics of supersonic submunition with parachute[J]. Acta Armamentrii,2011,32(5):520-525. (in Chinese)
[4]
Menter F R. Two-equation eddy-viscosity turbulence modelingfor engineering applications[J]. AIAA Journal, 1994, 32(8):1598-1605.
[5]
Weiss J M, Maruszewski J P, Smith W A. Implicit solution of preconditioned Navier-Stokes equations using algebraic multigrid[J]. AIAA Journal, 1999, 37(1):29-36.
[6]
Weiss J M, Smith W A. Preconditioning applied to variable and constant density flows[J]. AIAA Journal, 1995, 33(11):2050-2057.
[7]
Charwat A F, Roos J N, Deweg F C, et al. An investigation of separated flows-Part I: the pressure field[J]. Journal of Spacecraft, 1980, 17(2):123-128.
