Citation: | Miao Lei, Xie Bin, Li Jianqiang, Li Yaohua, Huang Cundong, Jia Wei, Ma Tao. Development and application of the measurement system for thrust vectoring tests at 2.4m×2.4m transonic wind tunnel[J]. JOURNAL OF MECHANICAL ENGINEERING, 2017, 31(6): 78-85. doi: 10.11729/syltlx20160105 |
[1] |
曲东才.推力矢量控制技术发展及关键技术分析[J].航空科学技术, 2002, (3):30-33. http://www.cqvip.com/QK/97819X/200203/6318569.html
Qu D C. Development for thrust vector control technology and analysis for critical technology[J]. Acronantical Science and Technology, 2002, (3):30-33. http://www.cqvip.com/QK/97819X/200203/6318569.html
|
[2] |
贾毅, 郑芳, 黄浩, 等.低速风洞推力矢量试验技术研究[J].实验流体力学, 2014, 28(6):92-97. http://www.syltlx.com/CN/abstract/abstract10796.shtml
Jia Y, Zheng F, Huang H, et al. Research on vectoring thrust test technology in low-speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(6):92-97. http://www.syltlx.com/CN/abstract/abstract10796.shtml
|
[3] |
Smith C L, Riddle T R. Jet effects testing considerations for the next-generation long-range strike aircraft[R]. AIAA-2008-1621, 2008. doi: 10.2514/6.2008-1621
|
[4] |
Crose J, Mack T, Marx D. NASA/MFSC nozzle test bed[R]. AIAA-89-2871, 1989. doi: 10.2514/6.1989-2871
|
[5] |
付尧明, 王强, 额日其太, 等.矢量喷管六分量测力试验台的研制[J].流体力学实验与测量, 2002, 16(1):87-93. http://d.wanfangdata.com.cn/Periodical/ltlxsyycl200201014
Fu Y M, Wang Q, Eriqitai, et al. Development of the six-component force-measuring balance for thrust-vectoring nozzle testing[J]. Experiments and Measurements in Fluid Mechanics, 2002, 16(1):87-93. http://d.wanfangdata.com.cn/Periodical/ltlxsyycl200201014
|
[6] |
贺伟, 童泽润, 李宏斌.单模块超燃发动机推力测量天平研制[J].航空动力学报, 2010, 25(10):2285-2289. http://www.cnki.com.cn/Article/CJFDTOTAL-DJZD201402033.htm
He W, Tong Z R, Li H B. Investigation of thrust balance for the single module scramjet[J]. Journal of Aerospace Power, 2010, 25(10):2285-2289. http://www.cnki.com.cn/Article/CJFDTOTAL-DJZD201402033.htm
|
[7] |
章荣平, 王勋年, 黄勇, 等.低速风洞全模TPS试验空气桥的设计与优化[J].实验流体力学, 2012, 26(6):48-52. http://www.syltlx.com/CN/abstract/abstract10476.shtml
Zhang R P, Wang X N, Huang Y, et al. Design and optimization of the air bridge for low speed full-span TPS test[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(6):48-52. http://www.syltlx.com/CN/abstract/abstract10476.shtml
|
[8] |
王超, 林俊.天平与波纹管系统结构设计与有限元分析[J].实验流体力学, 2013, 27(3):77-92. http://www.syltlx.com/CN/abstract/abstract10437.shtml
Wang C, Lin J. Structure design and finite element analysis on system of balance and bellows[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(3):77-92. http://www.syltlx.com/CN/abstract/abstract10437.shtml
|
[9] |
刘岩, 段玫, 张道伟.波纹管应力分析研究进展[J].管道技术与设备, 2006, (4):31-33. http://www.cqvip.com/QK/97879X/200604/22690496.html
Liu Y, Duan M, Zhang D W. Development of stress analysis of bellows[J]. Pipeline Technique and Equipment, 2006, (4):31-33. http://www.cqvip.com/QK/97879X/200604/22690496.html
|
[10] |
哈力旦·木沙, 买买提依明·艾尼.机械密封焊接金属波纹管膜片结构的有限元分析[J].新疆大学学报(自然科学版), 2007, 24(4):490-494. http://www.doc88.com/p-340625080328.html
Halidan Musha, Mamaitiming Aini. FEM analysis of metal welded bellow wave of mechanical seal[J]. Journal of Xinjiang University (Natural Science Edition), 2007, 24(4):490-494. http://www.doc88.com/p-340625080328.html
|
[11] |
刘高计, 谌满荣, 于卫青.风洞应变天平优化设计方法研究[J].弹箭与制导学报, 2006, 26(2):94-97. http://d.wanfangdata.com.cn/Periodical/djyzdxb200602033
Liu G J, Chen M R, Yu W Q. The research of optimum design method of strain-gauge balance in wind-tunnel[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2006, 26(2):94-97. http://d.wanfangdata.com.cn/Periodical/djyzdxb200602033
|
[12] |
Braman K B, Schweikhard W G, Yechout T R. Thrust modeling:A simplified in-flight thrust and airflow prediction technique for flight test performance measurements[R]. AIAA-83-2751, 1983. https://www.researchgate.net/publication/268462374_Thrust_modeling_-_A_simplified_in-flight_thrust_and_airflow_prediction_technique_for_flight_test_performance_measurements
|
[13] |
Wong K C. Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility[R]. NASA/TM 2003-212326. https://www.researchgate.net/publication/24293133_Derivation_of_the_Data_Reduction_Equations_for_the_Calibration_of_the_Six-Component_Thrust_Stand_in_the_CE-22_Advanced_Nozzle_Test_Facility
|
[14] |
Booth D, Ulbrich N. Calibration and data analysis of the MC-130 air balance[C]. 8th International Symposium on Strain-Gauge Balances, Ameron Hotel Flora, Lucerne, Switzerland, 2012. doi: 10.2514/6.2013-545
|