ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (6): 127072.doi: 10.7527/S1000-6893.2022.27072
• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles
Junhong LI1,2, Xuhong JIN1,2,3(
), Chunfeng LIU1, Wenbo MIAO1,2, Xiaoli CHENG1,2
Received:2022-02-24
Revised:2022-03-09
Accepted:2022-03-25
Online:2023-03-25
Published:2022-04-06
Contact:
Xuhong JIN
E-mail:jinxuhong08@163.com
Supported by:CLC Number:
Junhong LI, Xuhong JIN, Chunfeng LIU, Wenbo MIAO, Xiaoli CHENG. Microaerodynamic experiment and computation of near space high speed vehicles[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127072.
Table 2
Three test results of blunt cone micro aerodynamics
| 工况 | α/(°) | CN | CA | Cmz |
|---|---|---|---|---|
| 1 | -4 | -0.092 34 | 0.177 85 | 0.057 45 |
| -2 | -0.045 18 | 0.174 95 | 0.027 91 | |
| 0 | -0.001 78 | 0.172 86 | 0.001 22 | |
| 2 | 0.043 69 | 0.174 81 | -0.026 91 | |
| 4 | 0.095 82 | 0.182 53 | -0.059 61 | |
| 2 | -4 | -0.097 85 | 0.185 952 | 0.062 50 |
| -2 | -0.047 19 | 0.180 981 | 0.030 14 | |
| 0 | -0.000 73 | 0.178 416 | 0.000 51 | |
| 2 | 0.046 34 | 0.180 368 | -0.029 50 | |
| 4 | 0.099 53 | 0.186 346 | -0.063 70 | |
| 3 | -4 | -0.098 36 | 0.185 31 | 0.061 98 |
| -2 | -0.047 81 | 0.182 38 | 0.030 13 | |
| 0 | -0.000 65 | 0.181 59 | 0.000 39 | |
| 2 | 0.046 87 | 0.183 91 | -0.029 23 | |
| 4 | 0.100 03 | 0.187 78 | -0.063 50 |
| 1 | 于登云. 新型航天器发展对力学学科的挑战[J]. 科学通报, 2015, 60(12): 1085-1094. |
| YU D Y. Mechanical challenges in advanced spacecraft development[J]. Chinese Science Bulletin, 2015, 60(12): 1085-1094 (in Chinese). | |
| 2 | FREEMAN J D C, REUBUSH D E, MCCLINTON C R,et al. The NASA hyper-X program: NASA TM-1997-207243[R]. Washington, D. C.: NASA, 1997. |
| 3 | MORELLI E A, DERRY S D, SMITH M S. Aerodynamic parameter estimation for the X-43A(hyper-X)from flight data[C]∥ AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston: AIAA, 2005. |
| 4 | MARSHALL L A, BAHM C, CORPENING G P, et al. Overview with results and lessons learned of the X-43a Mach 10 flight[C]∥ AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Comference. Reston: AIAA, 2005. |
| 5 | 马汉东. 高超声速技术项目“Hyper-X”气动研究方法学[J]. 力学与实践, 2014, 36(3): 261-268, 277. |
| MA H D. Methodology of aerodynamic research for hypersonic technical project“Hyper-X”[J]. Mechanics in Engineering, 2014, 36(3): 261-268, 277 (in Chinese). | |
| 6 | BERRY S, DARYABEIGI K, WURSTER K, et al. Boundary layer transition on X-43A[C]∥ 38th Fluid Dynamics Conference and Exhibit. Reston: AIAA, 2008. |
| 7 | HANK J M. Air force research laboratory hypersonic propulsion research programs[C]∥ 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2007. |
| 8 | CANDLER G, JOHNSON H, ALBA C, et al. Analysis of modal growth on the leeward center plane of the X-51 vehicle: FRL-RB-WP-TM-2010-3001A[R]. Minnesota: University of Minnesota, 2010. |
| 9 | 李建林. 临近空间高超声速飞行器发展研究[M]. 北京:中国宇航出版社, 2012. |
| LI J L. Development survey of near space hypersonic vehicles[M]. Beijing: China Astronautic Publishing House, 2012 (in Chinese). | |
| 10 | WALKER S, SHERK J, SHELL D, et al. The DARPA/AF falcon program:the hypersonic technology vehicle #2 (HTV-2)flight demonstration phase[C]∥ 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2008. |
| 11 | WALKER S H, RODGERS F. Falcon hypersonic technology overview[C]∥ 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2005. |
| 12 | 聂万胜, 罗世彬, 丰松江, 等. 近空间飞行器关键技术及其发展趋势分析[J]. 国防科技大学学报, 2011, 34(2):107-113. |
| NIE W S, LUO S B, FENG S J,et al. Analysis of key technologies and development trend of near space vehicle[J]. Journal of National University of Defense Technology, 2011, 34(2): 107-113 (in Chinese). | |
| 13 | 陈冰, 郑勇, 陈张雷, 等. 临近空间高超声速飞行器天文导航系统综述[J]. 航空学报, 2020, 41(8): 623686. |
| CHEN B, ZHENG Y, CHEN Z L, et al. A review of celestial navigation system on near space hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(8): 623686 (in Chinese). | |
| 14 | 余平, 段毅, 尘军. 高超声速飞行的若干气动问题[J]. 航空学报, 2015, 36(1): 7-23. |
| YU P, DUAN Y, CHEN J. Some aerodynamic issues in hypersonic flight[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 7-23 (in Chinese). | |
| 15 | 叶友达, 张涵信, 蒋勤学, 等. 近空间高超声速飞行器气动特性研究的若干关键问题[J]. 力学学报, 2018, 50(6):1292-1310. |
| YE Y D, ZHANG H X, JIANG Q X, et al. Some key problems in the study of aerodynamic characteristics of near-space hypersonic vehicles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(6): 1292-1310 (in Chinese). | |
| 16 | 李廷伟, 张莽, 赵文文, 等. 面向稀薄流非线性本构预测的机器学习方法[J]. 航空学报, 2021, 42(4): 524386. |
| LI T W, ZHANG M, ZHAO W W, et al. Machine learning method for correction of rarefied nonlinear constitutive relations[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(4): 524386 (in Chinese). | |
| 17 | 程晓丽, 苗文博, 黄飞, 等. 跨流域多物理效应新型实验与预测技术[R]. 北京: 中国航天空气动力技术研究院, 2021. |
| CHENG X L, MIAO W B, HUANG F, et al. New experiment and computation technology for multi-physical effects in multiple flow regime[R]. Beijing: China Academy of Aerospace Aerodynamics, 2021 (in Chinese). | |
| 18 | 靳旭红, 黄飞, 程晓丽, 等. Maxwell气固相互作用模型对稀薄高超声速凹腔绕流流动特征和热环境的影响[J]. 航空学报, 2021, 42(3): 124118. |
| JIN X H, HUANG F, CHENG X L, et al. Effect of Maxwell gas surface interaction models on flow characteristics and thermodynamic properties of rarefied hypersonic cavity flows[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(3): 124118 (in Chinese). | |
| 19 | JIN X H, HUANG F, CHENG X L, et al. Monte Carlo simulation for aerodynamic coefficients of satellites in low-Earth orbit[J]. Acta Astronautica, 2019, 160(1): 222-229. |
| 20 | 刘春风, 刘家骅. 微量天平测力技术[R]. 北京: 中国航天空气动力技术研究院, 2021. |
| LIU C F, LIU J H. Microbalance force measurement technology[R]. Beijing: China Academy of Aerospace Aerodynamics, 2021 (in Chinese). | |
| 21 | 孙勇堂, 赵之平, 石运军, 等. CAAA新建Φ1.2米常规高超声速风洞[C]∥ 中国力学大会,2017. |
| SUN Y T, ZHAO Z P, SHI Y J, et al. New-built 1.2 diameter conventional hypersonic wind tunnel[C]∥ Chinese Mechanics Conference, 2017. | |
| 22 | 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 C. Computational fluid mechanics and methods[M]. Beijing: Beihang University Press, 2006 (in Chinese). | |
| 23 | 苗文博, 罗晓光, 程晓丽, 等. 壁面催化对高超声速飞行器气动特性影响[J]. 空气动力学学报, 2014, 32(2): 235-239. |
| MIAO W B, LUO X G, CHENG X L, et al. Surface recombination effects on aerodynamic loads of hypersonic vehicles [J]. Acta Aerodynamica Sinica, 2014, 32(2):235-239 (in Chinese). | |
| 24 | LIOU M S. A further development of the AUSM+ scheme towards robust and accurate solutions for all speeds[C]∥ 16th AIAA Computational Fluid Dynamics Conference. Reston: AIAA, 2003. |
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