Clark I G, Hutchings A L, Tanner C L, et al. Supersonic inflatable aerodynamic decelerators for use on future robotic missions to mars[C]//Proceedings of the IEEE Aerospace Conference Proceedings, Montana, USA: IEEE, 2008.
[2]
Brandon P S, Christopher L T, Milad M, et al. A historical review of inflatable aerodynamic decelerator technology development[C]//Proceedings of the IEEE Aerospace Conference Proceedings, Montana, USA: IEEE, 2010.
[3]
Anderson M S, Robinson J C, Bush H G, et al. A tension shell structure for application to entry vehicles, NASA TN D-2675[R]. Washington D.C.: NASA, 1965.
[4]
Braun R D, Manning R M. Mars exploration entry, descent, and landing challenges[J]. Journal of Spacecraft and Rockets, 2007, 44(2):310-323.
[5]
Clark I G, Cruz J R, Hughes M F, et al. Aerodynamic and aeroelastic characteristics of a tension cone inflatable aerodynamic decelerator[C]//Proceedings of the Aerodynamic Decelerator Systems Technology Conference and Seminar, AIAA. Washington: D.C.: AIAA, 2009.
[6]
阎超.计算流体力学方法及应用[M].北京:北京航空航天大学出版社, 2006. Yan Chao. Method and application of computational fluid dynamics[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2006. (in Chinese)
