Citation: | Lei Pengxuan, Wang Yuanjing, Lyu Binbin, Yu Li, Yang Zhenhua. Application of a smart material structure in the study of aerodynamic characteristics of a morphing wing[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(5): 74-80. DOI: 10.11729/syltlx20160166 |
[1] |
Wlezien R W, Horner G C, McGowan A M R, et al. Aircraft morphing program[C]//5th Annual International Symposium on Smart Structures and Materials, International Society for Optics and Photonics, 1998:176-187.
|
[2] |
Kudva J N. Overview of the DARPA smart wing project[J]. Journal of Intelligent Material Systems and Structures, 2004, 15(4):261-267. DOI: 10.1177/1045389X04042796
|
[3] |
Kudva J N, Jardine A P, Martin C A, et al. Overview of the ARPA/WL smart structures and materials development-smart wing contract[C]//1996 Symposium on Smart Structures and Materials, International Society for Optics and Photonics, 1996:10-16.
|
[4] |
Martin C A, Jasmin L, Flanagan J, et al. Smart wing wind tunnel model design[C]//Proc SPIE, 1997, 3044:41-47.
|
[5] |
Scherer L B, Martin C A, Appa K, et al. Smart wing wind tunnel test results[C]//Smart Structures and Materials'97, International Society for Optics and Photonics, 1997:56-66.
|
[6] |
Scherer L B, Martin C A, West M N, et al. DARPA/ARFL/NASA Smart Wing second wind tunnel test results[C]//1999 Symposium on Smart Structures and Materials, International Society for Optics and Photonics, 1999:249-259.
|
[7] |
Precup N, Mor M, Livne E. Design, construction, and tests of an aeroelastic wind tunnel model of a variable camber continuous trailing edge flap (VCCTEF) concept wing[R]. AIAA-2014-2442, 2014.
|
[8] |
Precup N, Mor M, Livne E. The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration[C]//56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2015. doi:10.2514/6.2015-1406.
|
[9] |
Ting E, Dao T, Nguyen N. Aerodynamic load analysis of a variable camber continuous trailing edge flap system on a flexible wing aircraft[C]//56th AIAA/ASCE/AHS/ASC Struc-tures, Structural Dynamics, and Materials Conference, 2015. doi:10.2514/6.2015-1839.
|
[10] |
陶宝祺.智能材料结构[M].北京:国防工业出版社, 1997.
Tao B Q. Intelligent material structure[M]. Beijing:National Defence Industry Press, 1997.
|
[11] |
Icardi U, Ferrero L. Preliminary study of an adaptive wing with shape memory alloy torsion actuators[J]. Materials & Design, 2009, 30(10):4200-4210. https://www.researchgate.net/publication/223715078_Preliminary_study_of_an_adaptive_wing_with_shape_memory_alloy_torsion_actuators
|
[12] |
Brailovski V, Terriault P, Georges T, et al. SMA actuators for morphing wings[J]. Physics Procedia, 2010, 10(12):197-203. https://www.researchgate.net/profile/Daniel_Coutu2/publication/251709682_SMA_Actuators_for_Morphing_Wings/links/561e6d1908aecade1accb598/SMA-Actuators-for-Morphing-Wings.pdf
|
[13] |
Coutu D, Brailovski V, Terriault P. Optimized design of an active extrados structure for an experimental morphing laminar wing[J]. Aerospace Science & Technology, 2010, 14(7):451-458. https://www.researchgate.net/publication/222536394_Optimized_design_of_an_active_extrados_structure_for_an_experimental_morphing_laminar_wing
|
[14] |
陈钱, 白鹏, 尹维龙, 等.可连续光滑偏转后缘的变弯度翼型气动特性分析[J].空气动力学学报, 2010, 28(1):46-53. http://www.cnki.com.cn/Article/CJFDTOTAL-KQDX201001006.htm
Chen Q, Bai P, Ying W L, et al. Analysis on the aerodynamic characteristics of variable camber airfoils with continuous smooth morphing trailing edge[J]. Acta Aerodynamica Sinica, 2010, 28(1):46-53. http://www.cnki.com.cn/Article/CJFDTOTAL-KQDX201001006.htm
|
[15] |
杨媛, 徐志伟.基于SMA的飞行器变体机翼驱动结构研究[J].兵器材料科学与工程, 2010, 33(1):25-30. http://www.cnki.com.cn/Article/CJFDTOTAL-BCKG201001014.htm
Yang Y, Xu Z W. Research of the wing structure based on a shape-memory alloy actuated morphing wing[J]. Ordnance Material Science and Engineering, 2010, 33(1):25-30. http://www.cnki.com.cn/Article/CJFDTOTAL-BCKG201001014.htm
|
[16] |
刘俊兵, 王帮峰, 芦吉云, 等.基于SMA的差动式变体机翼后缘驱动器研究[J].兵器材料科学与工程, 2015, 38(4):14-18. http://www.cnki.com.cn/Article/CJFDTOTAL-BCKG201504005.htm
Liu J B, Wang B F, Lu J Y, et al. Differential SMA actuator in trailing edge of morphing wing[J]. Ordnance Material Science and Engineering. 2015, 38(4):14-18. http://www.cnki.com.cn/Article/CJFDTOTAL-BCKG201504005.htm
|
[17] |
Burner A W, Liu T. Videogrammetric model deformation measurement technique[J]. Journal of Aircraft, 2001, 38(4):745-754. DOI: 10.2514/2.2826
|
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