Citation: | Xie Fei, Guo Leitao, Zhang Shaowu, Cao Cheng, Zou Qiongfen. Study on model base pressure measuring technique in hypersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043 |
[1] |
Michael R Mendenhall. 战术导弹空气动力学(下)[M]. 北京: 宇航出版社, 1999: 15-18.
|
[2] |
熊波, 林学东, 杨洋. 超声速风洞高马赫数模型底压精确测量研究[J]. 气动研究与发展, 2013, 23(3): 26-32. http://cdmd.cnki.com.cn/Article/CDMD-90002-1014047995.htm
Xiong B, Lin X D, Yang Y. A study on accurate measurement of bottom pressure at high Mach modelin supersonic wind tunnel[J]. Aerodynamics Research and Development, 2013, 23(3): 26-32. http://cdmd.cnki.com.cn/Article/CDMD-90002-1014047995.htm
|
[3] |
谭俊杰, 王福华, 张可忠, 等. 尾支杆对超音速弹丸底压测量的影响[J]. 兵工学报, 1997, 18(1): 89-92. http://www.cnki.com.cn/Article/CJFDTOTAL-BIGO199701020.htm
Tan J J, Wang F H, Zhang K Z, et al. The effect of tail sting on the base pressure measurement at supersonic velocities[J]. Acta Armamentarii, 1997, 18(1): 89-92. http://www.cnki.com.cn/Article/CJFDTOTAL-BIGO199701020.htm
|
[4] |
谭俊杰, 王福华, 徐琴, 等. 支杆及船尾对超声速弹丸底压影响的实验研究和理论计算[J]. 流体力学实验与测量, 1997, 11(4): 13-17. http://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199704003.htm
Tan J J, Wang F H, Xu Q, et al. The experimental investigation and analysis about the effects of tall sting and boat tail on the base pressure of projectiles at supersonic[J]. Experiments and Measurements in Fluid Mechanics, 1997, 11(4): 13-17. http://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199704003.htm
|
[5] |
James Despirito. Base pressure computations of the DERA generic missile wind tunnel model[R]. ARL-TR-3653, 2005. http://www.cnki.com.cn/Article/CJFDTOTAL-LTLC199704003.htm
|
[6] |
Moore F G, Moore L Y. Improvements to power-on base pressure prediction for the aeroprediction code[R]. AIAA 2010-664, 2010. DOI: 10.2514/MASM88
|
[7] |
Neiland V, Yereza A, Yermak Y. Investigation of turbine exhaust gas recirculation, base heating, and base pressure in the T-109 TsAGI wind tunnel for the IIAS ATLAS carrier model[R]. AIAA-95-6144, 1995.
|
[8] |
Mitchell R R, Webb M B. A study of the base pressure distribution of a slender body of square cross-section[R]. AIAA 2008-428, 2008. DOI: 10.2514/6.2008-428
|
[9] |
李其畅, 余立, 凌忠伟, 等. 高超声速气流下模型底部压力测量方法研究[C]//第十三届高超声速气动力(热)学术交流会议论文集, 2005.
|
[10] |
邹琼芬, 林敬周, 梁洁. 电子扫描压力测量系统设计[J]. 江汉大学学报, 2010, 38(1): 43-46. http://www.cnki.com.cn/Article/CJFDTOTAL-WHZG201001013.htm
|
[11] |
王冰, 尤彩红, 王文襄. 微型及超微型压力传感器的开发[J]. 仪表技术与传感器, 2009, (S): 180-181. http://www.cnki.com.cn/Article/CJFDTOTAL-YBJS2009S1060.htm
Wang B, You C H, Wang W X. Design of miniature and super-miniature pressure sensor[J]. Instrument Technique and Sensor, 2009, (S): 180-181. http://www.cnki.com.cn/Article/CJFDTOTAL-YBJS2009S1060.htm
|
[1] | XIA Huihui, ZHANG Shunping, YANG Shunhua, KAN Ruifeng, XU Zhenyu, RUAN Jun, YAO Lu, HUANG An. Two-dimensional distribution measurement of direct-connect scramjet combustion flow field based on TDLAS multi-absorption lines[J]. Journal of Experiments in Fluid Mechanics, 2025, 39(1): 80-86. DOI: 10.11729/syltlx20220103 |
[2] | CHENG Xiaoqi, FAN Ziye, TANG Zhanqi, BAI Jianxia, JIANG Nan. Experimental investigation of the spatial distribution of uniform momentum zones in wall-bounded flow[J]. Journal of Experiments in Fluid Mechanics, 2024, 38(4): 21-28. DOI: 10.11729/syltlx20230132 |
[3] | LI Long, PENG Lei, ZHAO Wei. Study of liquid spreading and particle size distribution during the preparation of aluminum alloy powder by rotary disc atomization[J]. Journal of Experiments in Fluid Mechanics. DOI: 10.11729/syltlx20230059 |
[4] | CHEN Shuyue, GUO Xiangdong, WANG Zixu, LIU senyun, WU Yingchun. Preliminary research on size measurement of supercooled large droplet in icing wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(3): 22-29. DOI: 10.11729/syltlx20200104 |
[5] | LI Fangji, ZHAO Qing, FAN Jianchao, JIA Shuang, RONG Xiangsen, GUO Min. Technology research and test verification of distributed flow regulator for inlet test in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(4): 74-80. DOI: 10.11729/syltlx20190022 |
[6] | Ma Wenyong, Wang Guanya, Zheng Xi, Chen Tie, Li Zhi, Zhang Chengyuan, Fang Pingzhi. Effects of end condition on aerodynamic force distribution on a skewed circular cylinder[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2): 43-50. DOI: 10.11729/syltlx20180050 |
[7] | Liu Lu, Cao Wei. Stability and transition prediction of the hypersonic plate boundary layers for wall temperature distribution[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(6): 41-48. DOI: 10.11729/syltlx20180107 |
[8] | Wu Liyin, Zhang Kouli, Li Chenyang, Li Qinglian. Model for three-dimensional distribution of liquid fuel in supersonic crossflows[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(4): 20-30. DOI: 10.11729/syltlx20170172 |
[9] | Zhang Jing, Zheng Xu, Wang Leilei, Cui Haihang, Li Zhanhua. Experimental study on the characteristic motion of bubble propelled hollow Janus microspheres[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(2): 61-66. DOI: 10.11729/syltlx20160152 |
[10] | An Yali, Xu Zhipeng, Liu Tiejun, Xie Dailiang. Experimental study on flowrate measurement of air-water two phase flow by double-cone flowmeter[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(5): 67-73. DOI: 10.11729/syltlx20160044 |
1. |
刘奇,刘常青,李增军. 超声速风洞模型冲击载荷抑制装置设计. 航空动力学报. 2023(02): 364-370 .
![]() | |
2. |
王珏,王誉超,季辰. 超声速风洞带舵机状态全尺寸舵颤振亚临界试验. 空天防御. 2023(02): 77-83 .
![]() | |
3. |
Chuanwei XUAN,Jinglong HAN,Bing ZHANG,Haiwei YUN,Xiaomao CHEN. Hypersonic flutter and flutter suppression system of a wind tunnel model. Chinese Journal of Aeronautics. 2019(09): 2121-2132 .
![]() |
|
4. |
周波,涂清,高川. 超声速风洞模型插入机构控制系统设计. 测控技术. 2019(12): 122-125+135 .
![]() | |
5. |
周波,高川,杨洋. 2m超声速风洞流场变速压控制方法研究. 实验流体力学. 2019(06): 72-77 .
![]() | |
6. |
季辰,赵玲,朱剑,刘子强,李锋. 高超声速风洞连续变动压舵面颤振试验. 实验流体力学. 2017(06): 37-44 .
![]() |