Citation: | TANG Jianping, WU Fuzhang, PU Lidong, ZENG Xian'ang, ZHANG Haiyou, ZHANG Lei. Development of a two degrees of freedom support system for full model gust tests[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(3): 94-99. DOI: 10.11729/syltlx20200062 |
[1] |
胡海岩, 赵永辉, 黄锐. 飞机结构气动弹性分析与控制研究[J]. 力学学报, 2016, 48(1): 1-27. DOI: 10.6052/0459-1879-15-423
HU H Y, ZHAO Y H, HUANG R. Studies on aeroelastic analysis and control of aircraft structures[J]. Chinese Journal of Theoretical and Applied Mechanics, 2016, 48(1): 1-27. doi: 10.6052/0459-1879-15-423
|
[2] |
SILVA W, VARTIO E, SHIMKO A, et al. Development of aeroservoelastic analytical models and gust load alleviation control laws of a SensorCraft wind-tunnel model using measured data[R]. AIAA-2006-1935, 2006. doi: 10.2514/6.2006-1935
|
[3] |
SCOTT R C, VETTER T K, PENNING K B, et al. Aeroservo-elastic testing of a sidewall mounted free flying wind-tunnel model[R]. AIAA-2008-7186, 2008. doi: 10.2514/6.2008-7186
|
[4] |
REICHENBACH E Y. Aeroservoelastic design and test validation of the Joined-Wing Sensorcraft[R]. AIAA-2008-7189, 2008. doi: 10.2514/6.2008-7189
|
[5] |
REICHENBACH E, CASTELLUCCIO M, SEXTON B. Joined-Wing Sensorcraft aeroservoelastic wind tunnel test program[R]. AIAA-2011-1956, 2011. doi: 10.2514/6.2011-1956
|
[6] |
SHARMA V, REICHENBACH E. Development of an innovative support system for Sensor Craft model[R]. AIAA-2011-1958, 2011. doi: 10.2514/6.2011-1958
|
[7] |
SCOTT R C, CASTELLUCCIO M A, COULSON D A, et al. Aeroservoelastic wind-tunnel tests of a free-flying, Joined-Wing SensorCraft model for gust load alleviation[R]. AIAA-2011-1960, 2011. doi: 10.2514/6.2011-1960
|
[8] |
SCOTT R C, VETTER T K, PENNING K B, et al. Aeroservoelastic testing of free flying wind tunnel models Part 1: A sidewall supported semispan model tested for gust load alleviation and flutter suppression[R]. NASA/TP-2013-218051, 2013.
|
[9] |
SCOTT R C, VETTER T K, PENNING K B, et al. Aeroservo-elastic testing of free flying wind tunnel models Part 2: A centerline supported fullspan model tested for gust load alleviation[R]. NASA/TP-2014-218170, 2014.
|
[10] |
金华, 王辉, 张海酉, 等. FL-13风洞突风发生装置研究[J]. 空气动力学学报, 2016, 34(1): 40-46. DOI: 10.7638/kqdlxxb-2015.0134
JIN H, WANG H, ZHANG H Y, et al. Investigation on gust response test apparatus in FL-13 wind tunnel[J]. Acta Aerodynamica Sinica, 2016, 34(1): 40-46. doi: 10.7638/kqdlxxb-2015.0134
|
[11] |
陈磊, 吴志刚, 杨超, 等. 多控制面机翼阵风减缓主动控制与风洞试验验证[J]. 航空学报, 2009, 30(12): 2250-2256. DOI: 10.3321/j.issn:1000-6893.2009.12.002
CHEN L, WU Z G, YANG C, et al. Active control and wind tunnel test verification of multi-control surfaces wing for gust alleviation[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2250-2256. doi: 10.3321/j.issn:1000-6893.2009.12.002
|
[12] |
杨俊斌, 吴志刚, 戴玉婷, 等. 飞翼布局飞机阵风减缓主动控制风洞试验[J]. 北京航空航天大学学报, 2017, 43(1): 184-192. DOI: 10.13700/j.bh.1001-5965.2016.0079
YANG J B, WU Z G, DAI Y T, et al. Wind tunnel test of gust alleviation active control for flying wing configuration aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1): 184-192. doi: 10.13700/j.bh.1001-5965.2016.0079
|
[13] |
唐建平, 杨远志, 梁鉴. 低速全模颤振试验悬挂支撑系统[J]. 实验流体力学, 2014, 28(4): 65-69. DOI: 10.11729/syltlx20130014
TANG J P, YANG Y Z, LIANG J. Floating suspension system for full model flutter tests at low speed[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(4): 65-69. doi: 10.11729/syltlx20130014
|
[14] |
杨希明, 刘南, 郭承鹏, 等. 飞行器气动弹性风洞试验技术综述[J]. 空气动力学学报, 2018, 36(6): 995-1008. DOI: 10.7638/kqdlxxb-2018.0039
YANG X M, LIU N, GUO C P, et al. A survey of aeroelastic wind tunnel testtechnology of flight vehicles[J]. Acta Aerodynamica Sinica, 2018, 36(6): 995-1008. doi: 10.7638/kqdlxxb-2018.0039
|
1. |
屈东胜,樊宏杰,刘连伟,陈洁,邹前进. 基于近红外光谱的超声速燃烧场气体参数测量研究. 光学学报. 2020(03): 198-205 .
![]() |