| Citation: | WEI Kai, XU Chen, YAN Qun, et al. Inversion test of rotating blade surface pressure[J]. Journal of Aerospace Power, 2023, 38（4）：949-954 doi: 10.13224/j.cnki.jasp.20220645
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In order to verify the inversion calculation method of the surface pressure of the rotating blade, an inversion test platform for the surface pressure of the rotating blade was built, and the inversion test for the surface pressure of a set of two-blade propellers was carried out. The far-field noise of the propeller was measured by a microphone array, and the static pressure on the blade surface was measured by a Kulite pressure sensor and an offline collector, and then compared with the calculated results. The results showed that under the working conditions studied, the calculated results were in good agreement with the experimental results, and the trend was basically the same; the error between the experimental results and the calculated results of two measuring points was within 1%, and the accuracy was very high; the contrast difference between the points was large, which was mainly caused by the installation process error of the pressure sensor.
| [1] |
胡骏. 航空叶片机原理[M]. 北京: 国防工业出版社, 2014.
|
| [2] |
张帅,张强波,董江,等. 考虑流固耦合效应的航空发动机风扇叶片应力数值模拟与试验测量研究[J]. 推进技术,2022,43(2): 331-340. doi: 10.13675/j.cnki.tjjs.200175
ZHANG Shuai,ZHANG Qiangbo,DONG Jiang,et al. Numerical simulation and experimental measurement of aero-engine fan blades stress considering influence of fluid-structure interaction[J]. Journal of Propulsion Technology,2022,43(2): 331-340. (in Chinese) doi: 10.13675/j.cnki.tjjs.200175
|
| [3] |
李萍,乔宝英,汪洋. 桨叶表面压力测量技术综述[J]. 直升机技术,2006,146(2): 58-61.
LI Ping,QIAO Baoying,WANG Yang. Overview of blade surface pressure measurement technology[J]. Helicopter Technique,2006,146(2): 58-61. (in Chinese)
|
| [4] |
阎超,于剑,徐晶磊. CFD模拟方法的发展成就与展望[J]. 力学进展,2011,41(5): 562-589. doi: 10.6052/1000-0992-2011-5-lxjzJ2010-082
YAN Chao,YU Jian,XU Jinglei. On the achievements and prospects for the methods of computational fluid dynamics[J]. Advances In Mechanics,2011,41(5): 562-589. (in Chinese) doi: 10.6052/1000-0992-2011-5-lxjzJ2010-082
|
| [5] |
王维,杨永,夏贞锋. 不同螺旋桨滑流数值模拟方法对比研究[J]. 航空计算技术,2012,42(5): 80-86. doi: 10.3969/j.issn.1671-654X.2012.05.020
WANG Wei,YANG Yong,XIA Zhenfeng. Study on comparison of different numerical simulation methods concerning propeller slipstream[J]. Aeronautical Computing Technique,2012,42(5): 80-86. (in Chinese) doi: 10.3969/j.issn.1671-654X.2012.05.020
|
| [6] |
战培国,杨炯. 国外风洞试验的新机制、新概念、新技术[J]. 流体力学实验与测量,2004,18(4): 1-6.
ZHAN Peiguo,YANG Jiong. New systems, concepts and techniques in the area of foreign wind tunnel test[J]. Experiments and Measurements in Fluid Mechanics,2004,18(4): 1-6. (in Chinese)
|
| [7] |
TAKAO M,HIDEYUKI K. Surface pressure measurement on a rotating blade of field horizontal axial wind turbine in yawed condition[J]. Mechanical Systems Machine Elements and Manufacturing,2005,48(1): 156-163.
|
| [8] |
王庆伟,刘波,薄相峰. 轴流压气机转子叶片表面静压分布实验[J]. 推进技术,2011,32(5): 611-616. doi: 10.13675/j.cnki.tjjs.2011.05.006
WANG Qingwei,LIU Bo,BO Xiangfeng. Experiment of the static pressure on the rotating blade surface in an axial compressor[J]. Journal of Propulsion Technology,2011,32(5): 611-616. (in Chinese) doi: 10.13675/j.cnki.tjjs.2011.05.006
|
| [9] |
王庆伟,刘波,侯为民. 压气机转子叶片表面动态压力测量的探索[J]. 航空动力学报,2010,25(10): 2327-2332. doi: 10.13224/j.cnki.jasp.2010.10.027
WANG Qingwei,LIU Bo,HOU Weimin. Tentative research about pressure measurement on one point of compressor rotor blade surface[J]. Journal of Aerospace Power,2010,25(10): 2327-2332. (in Chinese) doi: 10.13224/j.cnki.jasp.2010.10.027
|
| [10] |
梁晨,牛夕莹,林枫,等. 某型涡轮动叶气动性能的实验研究[J]. 热能与动力工程,2012,27(4): 405-410.
LIANG Chen,NIU Xiying,LIN Feng,et al. Tentative research about pressure measurement on one point of compressor rotor blade surface[J]. Journal of Engineering for Thermal Energy and Power,2012,27(4): 405-410. (in Chinese)
|
| [11] |
闫清东,宋泽民,魏巍. 液力变矩器导轮叶片表面压力测量与分析[J]. 机械工程学报,2019,55(10): 115-121. doi: 10.3901/JME.2019.10.115
YAN Qingdong,SONG Zeming,WEI Wei. Pressure measurement and analysis of stator blade surface of hydrodynamic torque converter[J]. Journal of Mechanical Engineering,2019,55(10): 115-121. (in Chinese) doi: 10.3901/JME.2019.10.115
|
| [12] |
江露生,曹亚雄,刘婷. 共轴刚性旋翼悬停状态桨叶表面压力测量试验与计算研究[J]. 北京航空航天大学学报,2021,47(12): 2484-2493. doi: 10.13700/j.bh.1001-5965.2020.0669
JIANG Lusheng,CAO Yaxiong,LIU Ting. Experiment and computational study on blade surface pressure measurement of coaxial rigid rotor in hovering state[J]. Journal of Beijing University of Aeronautics and Astronautics,2021,47(12): 2484-2493. (in Chinese) doi: 10.13700/j.bh.1001-5965.2020.0669
|
| [13] |
林敬周,解福田,钟俊. 高超声速风洞压敏漆试验技术[J]. 航空学报,2017,38(7): 120890.1-120890.9.
LIN Jingzhou,XIE Futian,ZHONG Jun. Pressure sensitive paint test technique in hypersonic wind tunnel[J]. Acta Aeronautica et Astronautica Sinica,2017,38(7): 120890.1-120890.9. (in Chinese)
|
| [14] |
LI X D, ZHOU S. An inversion model for subsonic moving sound source reconstruction[R]. AIAA 95-0120, 1995.
|
| [15] |
LI X D,ZHOU S. Spatial transformation of the discrete sound field from a propeller[J]. AIAA Journal,1996,34(6): 1097-1102. doi: 10.2514/3.13198
|
| [16] |
LUO J,LI X D. An inverse aeroacoustic problem on rotor wake/stator interaction[J]. Journal of Sound and Virbration,2002,254(2): 219-229. doi: 10.1006/jsvi.2001.3671
|
| [17] |
罗俊,李晓东. 转子/静子干涉气动声学反问题研究[J]. 航空动力学报,2001,16(2): 279-282. doi: 10.13224/j.cnki.jasp.2001.03.015
LUO Jun,LI Xiaodong. An inverse aeroacoustic problem on rotor/stator interaction[J]. Journal of Aerospace Power,2001,16(2): 279-282. (in Chinese) doi: 10.13224/j.cnki.jasp.2001.03.015
|
| [18] |
赵庆贺,李晓东. 悬停状态下旋翼噪声声源反演的正则化方法[J]. 航空动力学报,2019,34(4): 838-846. doi: 10.13224/j.cnki.jasp.2019.04.013
ZHAO Qinghe,LI Xiaodong. Regularization method for subsonic hovering rotor sound source reconstruction[J]. Journal of Aerospace Power,2019,34(4): 838-846. (in Chinese) doi: 10.13224/j.cnki.jasp.2019.04.013
|
| [19] |
乔渭阳, 王良锋. 航空发动机气动声学[M]. 西安: 西北工业大学出版社, 2016.
|
| [20] |
WILLIAMS F J E,HAWKINGS D I. Sound generated by turbulence and surface in arbirary motion[J]. Philosophical Transactions of the Royal Society of London,1969,264(5): 321-342.
|
| [21] |
FARASSAT F. Linear acoustic formulas for calculation of rotating blade noise[J]. AIAA Journal,1981,19(9): 1122-1130. doi: 10.2514/3.60051
|
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