Citation: | LIU J,SONG Y H,CHEN L,et al. Free oscillation dynamic derivative test technology of a short-blunt shape vehicle[J]. Journal of Experiments in Fluid Mechanics, 2021,35(6):66-72. doi: 10.11729/syltlx20210010 |
[1] |
WAY D W, POWELL R W, CHEN A, et al. Mars science laboratory: entry, descent, and landing system performance[C]//Proc of the 2007 IEEE Aerospace Conference. 2007. doi: 10.1109/AERO.2007.352821
|
[2] |
REICHENAU D E A. Aerodynamic characteristics of disk-gap-band parachutes in the wake of Viking entry forebodies at Mach numbers from 0.2 to 2.6[R]. AEDC-TR-72-78, 1972. doi: 10.21236/ad0746291
|
[3] |
Petrick D, Davis B, Peregino P, et al. An experimental approach to determine the flight dynamics of NASA's Mars Science Lab Capsule[R]. ARL-TR-6790, 2017.
|
[4] |
EDQUIST K T, HOLLIS B R. Mars science laboratory heatshield aerothermodynamics: design and reconstruction [R]. AIAA 2013-2781, 2013. doi: 10.2514/6.2013-2781
|
[5] |
ALKANDRY H, BOYD I, REED E, et al. Numerical study of hypersonic wind tunnel experiments for Mars entry aeroshells[R]. AIAA 2009-3918, 2009. doi: 10.2514/6.2009-3918
|
[6] |
YOSHINAGA T,TATE A,WATANABE M,et al. Orbital re-entry experiment vehicle ground and flight dynamic test results comparison[J]. Journal of Spacecraft and Rockets,1996,33(5):635-642. doi: 10.2514/3.26813
|
[7] |
赵梦熊. 载人飞船返回舱的再入气动环境[J]. 气动实验与测量控制,1995,9(4):1-7.
ZHAO M X. The aerodynamic and aerothermodynamic circumstances of capsule type re-entry vehicle[J]. Aerodynamic Experiment and Measurement & Control,1995,9(4):1-7.
|
[8] |
赵梦熊. 载人飞船返回舱的动稳定性[J]. 气动实验与测量控制,1995,9(2):1-8.
ZHAO M X. The dynamic stability characteristics of capsule type Re-entry vehicles[J]. Aerodynamic Experiment and Measurement & Control,1995,9(2):1-8.
|
[9] |
方方. 神舟飞船返回舱气动设计综述[J]. 航天器工程,2004,13(1):124-131. doi: 10.2514/3.26813
|
[10] |
马洋,张青斌,丰志伟. 大气环境对火星探测器气动特性影响分析[J]. 航天返回与遥感,2016,37(2):18-25. doi: 10.3969/j.issn.1009-8518.2016.02.003
MA Y,ZHANG Q B,FENG Z W. Influence of atmosphere condition on aerodynamic characteristics of Mars probe[J]. Spacecraft Recovery & Remote Sensing,2016,37(2):18-25. doi: 10.3969/j.issn.1009-8518.2016.02.003
|
[11] |
何开锋,和争春. 飞船返回舱跨声速全局稳定性研究[J]. 飞行力学,1999,17(3):34-38. doi: 10.3969/j.issn.1002-0853.1999.03.007
HE K F,HE Z C. The global stability analysis of reentry capsule transonic flight[J]. Flight Dynamics,1999,17(3):34-38. doi: 10.3969/j.issn.1002-0853.1999.03.007
|
[12] |
宋玉辉,陈农,秦永明. 亚跨超声速返回舱动稳定特性[J]. 航天返回与遥感,2014,35(2):31-38. doi: 10.3969/j.issn.1009-8518.2014.02.005
SONG Y H,CHEN N,QIN Y M. Sub-, trans- and super-sonic dynamic stability characteristics for reentry capsule[J]. Spacecraft Recovery & Remote Sensing,2014,35(2):31-38. doi: 10.3969/j.issn.1009-8518.2014.02.005
|
[13] |
刘伟,赵海洋,杨小亮. 返回舱动态稳定性分析及被动控制方法研究[J]. 中国科学G辑,2010,40(9):1156-1164.
LIU W,ZHAO H Y,YANG X L. Analysis of dynamic stability and research of passive control method for capsule[J]. Science in China (Series G),2010,40(9):1156-1164.
|
[14] |
张涵信,袁先旭,叶友达,等. 飞船返回舱俯仰振荡的动态稳定性研究[J]. 空气动力学学报,2002,20(3):247-259. doi: 10.3969/j.issn.0258-1825.2002.03.001
ZHANG H X,YUAN X X,YE Y D,et al. Research on the dynamic stability of an orbital reentry vehicle in pitching[J]. Acta Aerodynamica Sinica,2002,20(3):247-259. doi: 10.3969/j.issn.0258-1825.2002.03.001
|
[15] |
杨在山. 载人飞船返回舱的气动特性分析与外形设计[J]. 气动实验与测量控制,1996,10(4):12-18.
YANG Z S. The configuration and aerodynamic characteristics of manned re-entry capsules[J]. Aerodynamic Experiment and Measurement & Control,1996,10(4):12-18.
|
[16] |
贾区耀, 陈农, 杨益农, 等. 返回舱跨声速动稳定特性[C]//近代空气动力学研讨会论文集. 2005: 182-187.
|
[17] |
梁杰,李志辉,李齐,等. 返回舱再入跨流域气动及配平特性数值研究[J]. 空气动力学学报,2018,36(5):848-855. doi: 10.7638/kqdlxxb-2018.0128
LIANG J,LI Z H,LI Q,et al. Numerical simulation of aerodynamic and trim characteristics across different flow regimes for reentry module[J]. Acta Aerodynamica Sinica,2018,36(5):848-855. doi: 10.7638/kqdlxxb-2018.0128
|
[18] |
宋威,艾邦成,蒋增辉,等. 返回舱跨声速自由飞行的静动稳定性[J]. 实验流体力学,2019,33(4):89-94. doi: 10.11729/syltlx20180083
SONG W,AI B C,JIANG Z H,et al. Free flight static and dynamic aerodynamic characteristics for re-entry capsule at transonic speed[J]. Journal of Experiments in Fluid Mechanics,2019,33(4):89-94. doi: 10.11729/syltlx20180083
|
[19] |
周伟江. 返回舱自由振动跨声速非定常流场数值模拟[J]. 空气动力学学报,2000,18(1):46-51. doi: 10.3969/j.issn.0258-1825.2000.01.007
ZHOU W J. Numerical simulation of unsteady transonic flow around a free oscillating reentry vehicle[J]. Acta Aerodynamica Sinica,2000,18(1):46-51. doi: 10.3969/j.issn.0258-1825.2000.01.007
|
[20] |
胡静,宋玉辉,陈农,等. 返回舱动稳定特性风洞试验的影响参数[J]. 航天返回与遥感,2013,34(5):14-19. doi: 10.3969/j.issn.1009-8518.2013.05.003
HU J,SONG Y H,CHEN N,et al. Study of key parameters for dynamic stability of reentry capsule[J]. Spacecraft Recovery & Remote Sensing,2013,34(5):14-19. doi: 10.3969/j.issn.1009-8518.2013.05.003
|
[21] |
范洁川. 风洞试验手册[M]. 北京: 航空工业出版社, 2002: 430-440.
|
[22] |
USELTEM B L, WALLACE A R. Damping-in-pitch and drag characteristics of the Viking configuration at Mach numbers from 1.6 through 3[R]. AEDC-TR-72-56, 1972.
|
[23] |
USELTON B L, SHADOW T O, MANSFIELD A C. Damping in pitch derivatives of 120 and 140 degree blunted cones at Mach numbers of 0.3 through 3[R]. AEDC-TR-70-49, 1972.
|