| [1] Korzun A M, Dubos G F, Iwata C K, et al. A concept for the entry, descent, and landing of high-mass payloads at Mars[J]. Acta Astronautica, 2010, 66(7): 1146-1159.[2] Hillje E R. Entry aerodynamics at Lunar return conditions, NASA TN-D-5399[R]. Washington, D.C.: NASA, 1969.[3] Tancredi U, Accardo D, Grassi M, et al. Unmanned space vehicle technology demonstrator[J]. Acta Astronautica, 2007, 60: 186-197.[4] Kinney D J. Development of the ORION crew exploration vehicle's aerothermal database using a combination of high fidelity CFD and engineering level methods, AIAA-2009-1100[R]. Reston: AIAA, 2009.[5] Kawato H, Watanabe S, Yamamoto Y, et al. Aerodynamic performances of lifting-body configurations for a reentry vehicle[J]. Journal of Spacecraft and Rockets, 2005, 42(2): 232-239.[6] Pardini C, Anselmo L, Moe K, et al. Drag and energy accommodation coefficients during sunspot maximum[J]. Advances in Space Research, 2010, 45(5): 638-650.[7] Vallado D A, Finkleman D. A critical assessment of satellite drag and atmospheric density modeling[J]. Acta Astronautica, 2014, 95: 141-165.[8] Martin A, Boyd I. Assessment of carbon-phenolic-in-air chemistry models for atmospheric re-entry, AIAA-2010-4656[R]. Reston: AIAA, 2010.[9] Zhuang F G, Cui E J, Zhang H X. Some developments and future air space vehicle dynamics task[C]//China First Modern Aerodynamics and Thermodynamics Pneumatic Conference Proceedings: Book 1. Beijing: National Defense Industry Press, 2006: 1-12 (in Chinese). 庄逢甘, 崔尔杰, 张涵信. 未来空间飞行器的某些发展和空气动力学的任务[C]//中国第一届近代空气动力学与气动热力学会议论文集: 上册. 北京: 国防工业出版社, 2006: 1-12.[10] Li Y L, Qi F R. Optimigation and implementation of China SHENZHOU spaceship's system and return technology scheme[J]. Spacecraft Recovery & Remote Sensing, 2012, 32(6): 1-13 (in Chinese). 李颐黎, 戚发韧. "神舟号"飞船总体与返回方案的优化与实施[J]. 航天返回与遥感, 2012, 32(6): 1-13.[11] Liang J, Li Z H, Du B Q. Research on trim features of reentry capsule in hypersonic rarefied flow regime[J]. Spacecraft Recovery & Remote Sensing, 2013, 34(3): 42-48 (in Chinese). 梁杰, 李志辉, 杜波强. 飞船返回舱再入稀薄流域配平特性研究[J]. 航天返回与遥感, 2013, 34(3): 42-48.[12] Fang F. A comprehensive analysis of re-entry capsule's aerodynamic design for SHENZHOU spaceship[J]. Spacecraft Engineering, 2004(1): 124-131 (in Chinese). 方方. 神舟飞船返回舱气动设计综述[J]. 航天器工程, 2004(1): 124-131.[13] Andrushchenko V A, Syzranova N G, Shevelev Y D. An estimate of the heat fluxes to the surface of blunt bodies moving at hypersonic velocity in the atmosphere[J]. Journal of Applied Mathematics and Mechanics, 2007, 71(5): 747-754.[14] Shang J S, Surzhikov S T. Simulating stardust Earth reentry with radiation heat transfer[J]. Journal of Spacecraft and Rockets, 2011, 48(3): 385-396.[15] Sarma G S R. Physico-chemical modelling in hypersonic flow simulation[J]. Progress in Aerospace Sciences, 2000, 36(3-4): 281-349.[16] Bityurin V A, Bocharov A N. Study of catalytic effects at reentry vehicle-MHD heat flux mitigation in irradiative hypersonic flow around a blunt body with ablating carbon surface, AIAA-2014-1033[R]. Reston: AIAA, 2014.[17] Zhao M X. Manned spacecraft aerodynamics[M]. Beijing: National Defense Industry Press, 2000: 86-90 (in Chinese). 赵梦熊. 载人飞船空气动力学[M]. 北京: 国防工业出版社, 2000: 86-90.[18] Li Z H, Zhang H X. Gas-kinetic numerical studies of three-dimensional complex flows on spacecraft re-entry[J]. Journal of Computational Physics, 2009, 228(4): 1116-1138.[19] Huang Z C. Missiles and space series: aerospace aerodynamics[M]. Beijing: China Aerospace Press, 1994: 50-62(in Chinese). 黄志澄. 导弹与航天丛书: 航天空气动力学[M]. 北京:宇航出版社, 1994: 50-62.[20] Whitehead A, Jr. NASP aerodynamics, AIAA-1989-5013[R]. Reston: AIAA, 1989.[21] Fang F. Manned spacecraft hypersonic flow field characteristics[C]//China-Russia Hypersonic Exchange Meeting. Beijing: China Great Wall Inductry Coperation, 2002 (in Chinese). 方方. 载人飞船航天器高超声速流场特性[C]//中俄高超声速交流会议. 北京: 中国长城工业有限公司, 2002.[22] Bertin J J, Cummings R M. Fifty years of hypersonics: where we've been, where we're going[J]. Progress in Aerospace Sciences, 2003, 39(6): 511-536.[23] Fu D X. Missiles and space series: computational aerodynamics[M]. Beijing: China Aerospace Press, 1994: 75-82 (in Chinese). 傅德薰. 导弹与航天丛书:计算空气动力学[M]. 北京: 中国宇航出版社, 1994: 75-82.[24] Jia Q Y, Fang F, Chen N, et al. Nonlinear aerodynamic resilience and aerocraft dynamic stability[J]. Acta Aerodynamica Sinica, 2003, 21(4): 446-448 (in Chinese). 贾区耀, 方方, 陈农, 等. 非线性气动恢复力与飞行器动稳定性[J]. 空气动力学学报, 2003, 21(4): 446-448.[25] Zhang H X, Yuan X X, Xie Y F, et al. Study of the dynamic stability of a pitching unfinned reentry capsule[J]. Acta Aerodynamica Sinica, 2004, 22(2): 130-134 (in Chinese). 张涵信, 袁先旭, 谢昱飞, 等. 不带稳定翼飞船返回舱俯仰动稳定性研究[J]. 空气动力学学报, 2004, 22(2): 130-134.[26] Schaaf S A, Chamber P L. "Fundamentals of gas dynamics" H articles "rarefied gas flows"[M]. Xu H F, translated. Beijing: Science Press, 1988: 31-37 (in Chinese). 沙夫S A, 钱伯P L. 《气体动力学基本原理》H篇"稀薄气体的流动"[M]. 徐华舫, 译. 北京: 科学出版社, 1988: 31-37.[27] Li Z H, Wu Z Y. DSCM simulation of hypersonic rarefied flow past Apollo-MC[J]. Acta Aerodynamica Sinica, 1996, 14(2): 230-233 (in Chinese). 李志辉, 吴振宇. 阿波罗指令舱稀薄气体动力学特征的蒙特卡罗数值模拟[J]. 空气动力学学报, 1996, 14(2): 230-233.[28] Liu W, Zhao H Y. Exploration of return capsule dynamic stability interdisciplinary research methods [C]//Seventh National Conference on Fluid Mechanics. Guilin: National Computational Fluid Dynamics Conference Organizing Committee, 2012: CSTM 2012-B03-0197 (in Chinese). 刘伟, 赵海洋. 返回舱动态稳定性多学科交叉研究方法探索[C]//第七届全国流体力学学术会议. 桂林: 全国计算流体力学会议组委会, 2012: CSTM 2012-B03-0197.[29] Reynier P. Survey of convective blockage for planetary entries[J]. Acta Astronautica, 2013, 83: 175-195. |
CJA
