Optics and Precision Engineering, Volume. 24, Issue 9, 2262(2016)
Optimization and experiments of deployment performance for folding wing mechanism of an aircraft
[1] [1] ZHOU Y, ZHOU X B, WANG Z Y.“Gem” laser guided bombs and wind and rain forty years [J].Weapon Expo., 2006(2): 5-9.(in Chinese)
[2] [2] DING H.Finite Element Analysis and Ex Perimental Study for Afolding Wing of Aircraftmissiles [D].Harbin: Harbin Engineering University, 2010.(in Chinese)
[5] [5] ROBERT K. Wing mechanism analysis [J]. Computers and Structures, 1999, 72(8): 253-265.
[6] [6] YUDI H, HOON C P, NAM S G. Byun Design and demonstration of a small expandable morphing wing [J]. Proc.of SPIE, 2005, 57(14): 224-231.
[7] [7] METOM S.Piezoelectrically actuated four-bar mechanism with two flexible links for micromechanical flying insect thorax [J].IEEE/ASME Transactions on Mechatronics, 2003, 104(1): 299-305.
[8] [8] MA C X, YU X D, WANG T.Missile folding wing exercise testing [J].Journal of Projectiles, Rockets, MissilesandGuidance, 1993(2): 63-65.(in Chinese)
[9] [9] LI X H, LI H N, WU J Q.Calculation and experimental study on the folding wing of rocket projectile [J]. Spacecraft Environment Engineering, 2009, 26: 82-86.(in Chinese)
[10] [10] CUI E W, YU C G, LI M, et al..The simulation analysis of the wing of a missile folding wing [J].Ordnance Industry Automation, 2013, 32(12): 12-15.(in Chinese)
[11] [11] WU J Q, SUN H W, ZHANG X.The researchon unfolding testand dynamic model of folding-wing [J]. Journal of Projectiles, Rockets, MissilesandGuidance, 2012, 32(3): 164-167.(in Chinese)
[12] [12] ZHAO J F, LIU L. Dynamic simulation and optimization design of folding wing deployment [J]. Journal of Projectiles, Rockets, MissilesandGuidance, 2011, 31(5): 141-146.(in Chinese)
[13] [13] CLOUGH R W, PENZIEN J, WANG G Y(Translation).Structural Dynamics [M]. Beijing: Higher Education Press, 2006.(in Chinese)
[15] [15] ZHENG L M, DENG CH P, YANG ZH H.Dynamic simulation and application of deployable mechanism of satellite solar panels [J]. Opt. Precision Eng., 2009, 17(12): 3047-3054.(in Chinese)
[17] [17] HUANG R Z, WAN J Q, MA H W.Optimization of synthetic culture condition ofcellulose producing strains using orthogonal experimental design [J].China Environmental Science, 2012, 32(1): 130-135.(in Chinese)
[18] [18] LIU G H, LIU W, LIU ZH. Using the four factor three level orthogonal regression analysis method to study the prediction of drilling string [J].Journal of Oil and Gas Technology, 2010, 32(3): 108-112.(in Chinese)
Get Citation
Copy Citation Text
HAN Xue-feng, LIU Xiao-dong, MA Wu-yuan, MA Qing, YUAN Dong-ming. Optimization and experiments of deployment performance for folding wing mechanism of an aircraft[J]. Optics and Precision Engineering, 2016, 24(9): 2262
Category:
Received: Jan. 17, 2016
Accepted: --
Published Online: Nov. 14, 2016
The Author Email: Xue-feng HAN (hanxuefeng5210@163.com)