Citation: | CHEN Z Y,LIU Y,XU L. Wind tunnel test investigation on buffeting characteristics of horizontal tail of commercial aircraft in low-speed cruise configuration[J]. Journal of Experiments in Fluid Mechanics, 2021,35(6):94-99.. DOI: 10.11729/syltlx20210009 |
[1] |
MABEY D G. Some aspects of aircraft dynamic loads due to flow separation[J]. Progress in Aerospace Sciences,1989,26(2):115-151. doi: 10.1016/0376-0421(89)90006-7
|
[2] |
ZAN S J,MAULL D J. Buffet excitation of wings at low speeds[J]. Journal of Aircraft,1992,29(6):1137-1143. doi: 10.2514/3.46296
|
[3] |
FLYNN G A,MORRISON J F,MABEY D G. Buffet alleviation on swept and unswept wings at high incidence[J]. Journal of Aircraft,2001,38(2):368-378. doi: 10.2514/2.2771
|
[4] |
王巍,杨智春,张新平. 扰流激励下垂尾抖振响应主模态控制风洞试验研究[J]. 振动与冲击,2012,31(16):18-21. DOI: 10.3969/j.issn.1000-3835.2012.16.004
WANG W,YANG Z C,ZHANG X P. Fin buffeting alleviation in disturbed flow by buffeting principal modal control method[J]. Jour-nal of Vibration and Shock,2012,31(16):18-21. doi: 10.3969/j.issn.1000-3835.2012.16.004
|
[5] |
张庆,叶正寅. 一种基于充气气囊的垂尾抖振抑制新方法研究[J]. 工程力学,2014,31(12):234-240. DOI: 10.6052/j.issn.1000-4750.2013.06.0564
ZHANG Q,YE Z Y. Study on a new method for suppression of vertical tail buffeting using inflatable bumps[J]. Engineering Mecha-nics,2014,31(12):234-240. doi: 10.6052/j.issn.1000-4750.2013.06.0564
|
[6] |
韩冰,徐敏,蔡天星,等. 涡破裂诱导的垂尾抖振数值模拟[J]. 航空学报,2012,33(5):788-795.
HAN B,XU M,CAI T X,et al. Numerical simulation of vertical tail buffeting induced by vortex breakdown[J]. Acta Aeronautica et As-tronautica Sinica,2012,33(5):788-795.
|
[7] |
ZHANG Q,YE Z Y. Novel method based on inflatable bump for vertical tail buffeting suppression[J]. Journal of Aircraft,2015,52 (1): 367-371. doi: 10.2514/1.c032552
|
[8] |
FERMAN M A,HUTTSELL L J,TURNER E W. Experiments with tangential blowing to reduce buffet response on an F-15 model[J]. Journal of Aircraft,2004,41(4):903-910. doi: 10.2514/1.290
|
[9] |
SHETA E, ROCK S, HUTTSELL L. Characteristics of vertical tail buffet of F/A-18 aircraft[C]//Proc of the 39th Aerospace Sciences Meeting and Exhibit. 2001. doi: 10.2514/6.2001-710
|
[10] |
ZHAO Y H,HU H Y. Active control of vertical tail buffeting by piezoelectric actuators[J]. Journal of Aircraft,2009,46(4):1167-1175. doi: 10.2514/1.39464
|
[11] |
HAUCH R M,JACOBS J H,DIMA C,et al. Reduction of vertical tail buffet response using active control[J]. Journal of Aircraft,1996,33(3):617-622. doi: 10.2514/3.46990
|
[12] |
ZHANG Q,HUA R H,YE Z Y. Experimental and computational investigation of novel vertical tail buffet suppression method for high sweep delta wing[J]. Science China Technological Sciences,2015,58(1):147-157. doi: 10.1007/s11431-014-5702-2
|
[13] |
RICCI S, BERETTA J, FONTE F, et al. Buffet load alleviation on the fin of a high performance training aircraft[C]//Proc of the 58th AIAA/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2017. doi: 10.2514/6.2017-1819.
|
[14] |
PETTIT C L,BROWN D L,BANFORD M P,et al. Full-scale wind-tunnel pressure measurements of an F/A-18 tail during buffet[J]. Journal of Aircraft,1996,33(6):1148-1156. doi: 10.2514/3.47069
|
[15] |
ELMEKAWY A,KANDIL O A,BAYSAL O. F/A-18 twin-tail buffet modeling using nonlinear eddy viscosity models[J]. Journal of Air-craft,2015,53(4):1106-1112. doi: 10.2514/1.C033482
|
[16] |
CANDON M J, LEVINSKI O, ALTAF A, et al. Aircraft transonic buffet load prediction using artificial neural networks[C]//Proc of the AIAA Scitech 2019 Forum. 2019. doi: 10.2514/6.2019-0763
|
[17] |
高杰,张明禄,吕志咏. 双立尾和三角翼之间的气动干扰实验研究[J]. 实验流体力学,2005,19(3):51-57. DOI: 10.3969/j.issn.1672-9897.2005.03.011
GAO J,ZHANG M L,LU Z Y. Investigation of aerodynamic interference between delta wings and twin fins[J]. Journal of Experi-ments in Fluid Mechanics,2005,19(3):51-57. doi: 10.3969/j.issn.1672-9897.2005.03.011
|
[18] |
ZIMMERMAN N, FERMAN M, YURKOVICH R, et al. Prediction of tail buffet loads for design application[C]//Proc of the 30th Struc-tures, Structural Dynamics and Materials Conference. 1989. doi: 10.2514/6.1989-1378
|
[19] |
MEYN L A,JAMES K D. Full-scale wind-tunnel studies of F/A-18 tail buffet[J]. Journal of Aircraft,1996,33(3):589-595. doi: 10.2514/3.46986
|
[20] |
ANDERSON W D,PATEL S R,BLACK C L. Low speed wind tunnel buffet testing on the F/A-22[J]. Journal of Aircraft,2006,43(4):879-885. doi: 10.2514/1.10247
|
[21] |
DANOWSKY B P, SCHULZE P C. Control surface buffet load measurement using aircraft actuators[C]//Proc of the AIAA Atmos-pheric Flight Mechanics Conference. 2016. doi: 10.2514/6.2016-2005
|
[22] |
管德. 气动弹性试验[M]. 北京: 北京航空学院出版社, 1986.
|
[23] |
ILLI S, FINGSKES C, LUTZ T, et al. Transonic tail buffet simulations for the common research model[C]//Proc of the 31st AIAA Applied Aerodynamics Conference. 2013. doi: 10.2514/6.2013-2510
|