Citation: | Song Wei, Ai Bangcheng, Jiang Zenghui, 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 |
[1] |
纪楚群, 周伟江.钟形返回舱空气动力特性数值模拟[J].航天返回与遥感, 2001, 22(1):32-37. doi: 10.3969/j.issn.1009-8518.2001.01.007
Ji C Q, Zhou W J. A numerical simulation of aerodynamic characters for bell capsule[J]. Spacecraft Recovery & Remote Sensing, 2001, 22(1):32-37. doi: 10.3969/j.issn.1009-8518.2001.01.007
|
[2] |
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. http://www.cnki.com.cn/Article/CJFDTotal-LTLC502.000.htm
Zhao M X. The dynamic stability characteristics of capsule type re-entry vehicles[J]. Aerodynamic Experiment and Measurement & Control, 1995, 9(2):1-8. http://www.cnki.com.cn/Article/CJFDTotal-LTLC502.000.htm
|
[3] |
陈河梧.飞船返回舱高超声速气动特性的风洞实验分析[J].航天器工程, 2008, 17(5):77-81. doi: 10.3969/j.issn.1673-8748.2008.05.014
Chen H W. Wind-tunnel test analysis on hypersonic aero-dynamic characteristics of returnable module[J]. Spacecraft Engineering, 2008, 17(5):77-81. doi: 10.3969/j.issn.1673-8748.2008.05.014
|
[4] |
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
|
[5] |
袁先旭, 张涵信, 谢昱飞.飞船返回舱再入俯仰动稳定吸引子数值仿真[J].空气动力学学报, 2007, 25(4):431-436. doi: 10.3969/j.issn.0258-1825.2007.04.004
Yuan X X, Zhang H X, Xie Y F. Numerical simulation for dynamic stability in pitching of unfinned reentry capsule and bifurcation with Mach number prediction[J].Acta Aerodynamica Sinica, 2007, 25(4):431-436. doi: 10.3969/j.issn.0258-1825.2007.04.004
|
[6] |
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
|
[7] |
Abe T, Sato S, Matsukawa Y, et al. Study for dynamically unstable motion of reentry capsule[R]. AIAA-2000-2589, 2000.
|
[8] |
Susumu T, Kozo F. Study on the mechanism of the instability of a re-entry capsule at transonic speeds[R]. AIAA-2000-2603, 2000.
|
[9] |
Susumu T, Kouju H, Kozo F. Numerical analysis of dynamic stability of a reentry capsule at transonic speed[J]. AIAA Journal, 2001, 39(4):646-653. doi: 10.2514/2.1357
|
[10] |
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:物理学力学天文学, 2010, 40(9):1156-1164. http://www.cnki.com.cn/Article/CJFDTotal-JGXK201009012.htm
Liu W, Zhao H Y, Yang X L. Analysis of dynamic stability and research of passive control method for capsule[J]. Scientia Sinica Physica, Mechanica & Astronomica, 2010, 40(9):1156-1164. http://www.cnki.com.cn/Article/CJFDTotal-JGXK201009012.htm
|
[11] |
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
|
[12] |
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
|
[13] |
Mitcheltree R A, Fremaux C M, Yates L A. Subsonic static and dynamic aerodynamics of blunt entry vehicles[R]. AIAA-99-1020, 1999.
|
[14] |
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
|
[15] |
Chapman G T, Mitcheltree R A, Hathaway W H. Transonic and low supersonic static and dynamic aerodynamic charac-teristics of the stardust sample return capsule[R]. AIAA-99-1021, 1999.
|
[16] |
Sommer S C, Compton D L, Short B J. Free-flight measurements of static and dynamic stability of models of the Project Mercury re-entry capsule at Mach numbers 3 and 9.5[R]. NASA TM X-373, 1960.
|
[17] |
Schoenenberger M, Hathaway W, Yates L, et al. Ballistic range testing of the Mars Exploration Rover entry capsule[R]. AIAA-2005-55, 2005.
|
[18] |
Schoenenberger M, Yates L, Hathaway W. Dynamic stability testing of the Mars Science Laboratory entry capsule[R]. AIAA-2009-3917, 2009.
|
[19] |
Cheatwood F M, Winchenbach G L, Hathaway W, et al. Dynamic stability testing of the genesis sample return capsule[R]. AIAA-2000-1009, 2000.
|
[20] |
苑朝凯, 孙英英, 姜宗林.高超声速脉冲风洞模型自由飞试验技术[J].气体物理, 2016, 1(2):55-63. http://d.old.wanfangdata.com.cn/Periodical/qtwl201602007
Yuan C K, Sun Y Y, Jiang Z L. Free flight test in hypersonic impulse wind tunnel[J]. Physics of Gases, 2016, 1(2):55-63. http://d.old.wanfangdata.com.cn/Periodical/qtwl201602007
|
[21] |
马家欢, 唐宗衡, 张小平, 等.激波管风洞中锥模型静、动稳定性导数的测量[J].力学学报, 1980, 16(1):84-89. http://www.cnki.com.cn/Article/CJFDTotal-LXXB198001009.htm
Ma J H, Tang Z H, Zhang X P, et al. The measurement of the static and dynamic stability derivatives of conical models in the shock tunnel[J]. Chinese Journal of Theoretical and Applied Mechanics, 1980, 16(1):84-89. http://www.cnki.com.cn/Article/CJFDTotal-LXXB198001009.htm
|
[22] |
宋威, 蒋增辉, 贾区耀.细长锥边界层绊线转捩风洞自由飞试验[J].力学学报, 2006, 48(6):1301-1307. http://d.old.wanfangdata.com.cn/Periodical/lxxb201606005
Song W, Jiang Z H, Jia Q Y. Wind-tunnel free-flight test of boundary layer transition induced by tripped thread for slender cone[J]. Chinese Journal of Theoretical and Applied Mechanics, 2006, 48(6):1301-1307. http://d.old.wanfangdata.com.cn/Periodical/lxxb201606005
|
[23] |
蒋增辉, 宋威, 陈农.小迎角高超声速非旋转钝锥非线性运动分析[J].航空学报, 2016, 37(5):1454-1461. http://d.old.wanfangdata.com.cn/Periodical/hkxb201605006
Jiang Z H, Song W, Chen N. Analysis of nonlinear motion for hypersonic non-spinning blunt cones at small angle of attack[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(5):1454-1461. http://d.old.wanfangdata.com.cn/Periodical/hkxb201605006
|
[24] |
Chapman G T, Kirk D B. A new method for extracting aerodynamics coefficients from free-flight data[R]. AIAA-69-134, 1969.
|