Optics and Precision Engineering, Volume. 28, Issue 10, 2244(2020)
Optimization of single lenticular honeycomb boom for optical film deployable mechanism
[4] [4] DING X L, LI X. Design of a type of deployable/retractable mechanism using friction self-locking joint units[J]. Mechanism and Machine Theory, 2015, 92: 273-288.
DING X L, LI X. Design of a type of deployable/retractable mechanism using friction self-locking joint units[J]. Mechanism and Machine Theory, 2015, 92: 273-288.
[5] [5] GAO M X. The Design of Deployable Mechanisms of Space Large Aperture Optical Primary Mirror[D]. Harbin: Harbin Institute of Technology, 2016.(in Chinese)
GAO M X. The Design of Deployable Mechanisms of Space Large Aperture Optical Primary Mirror[D]. Harbin: Harbin Institute of Technology, 2016.(in Chinese)
[6] [6] WANG CH L. Mechanism Design and Analysis of Space Large Aperture Deployable Membrane Optical Imager[D]. Harbin: Harbin Institute of Technology, 2017.(in Chinese)
WANG CH L. Mechanism Design and Analysis of Space Large Aperture Deployable Membrane Optical Imager[D]. Harbin: Harbin Institute of Technology, 2017.(in Chinese)
[7] [7] MURPHEY T. Historical perspectives on the development of deployable reflectors[C].50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Palm Springs, California. Reston, Virigina: AIAA, 2009.
MURPHEY T. Historical perspectives on the development of deployable reflectors[C].50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Palm Springs, California. Reston, Virigina: AIAA, 2009.
[8] [8] BAI J B, SHENOI R A, XIONG J J. Thermal analysis of thin-walled deployable composite boom in simulated space environment[J]. Composite Structures, 2017, 173: 210-218.
BAI J B, SHENOI R A, XIONG J J. Thermal analysis of thin-walled deployable composite boom in simulated space environment[J]. Composite Structures, 2017, 173: 210-218.
[9] [9] STABILE A, LAURENZI S. Coiling dynamic analysis of thin-walled composite deployable boom[J]. Composite Structures, 2014, 113: 429-436.
STABILE A, LAURENZI S. Coiling dynamic analysis of thin-walled composite deployable boom[J]. Composite Structures, 2014, 113: 429-436.
[10] [10] CAI Q Y, CHEN W J, ZHANG D X, et al.. Numerical simulation and experimental analysis of squashing and stretching of thin-walled tubular space extension arm [C] . 2014 Conference on Space Structure. The Chinese Society of Theoretical and Applied Mechanics, 2014. (in Chinese)
CAI Q Y, CHEN W J, ZHANG D X, et al.. Numerical simulation and experimental analysis of squashing and stretching of thin-walled tubular space extension arm [C] . 2014 Conference on Space Structure. The Chinese Society of Theoretical and Applied Mechanics, 2014. (in Chinese)
[11] [11] HU Y, CHEN W J, LI R X, et al.. Mechanical characteristics of deployable composite thin-walled lenticular tubes[J]. Composite Structures, 2016, 153: 601-613.
HU Y, CHEN W J, LI R X, et al.. Mechanical characteristics of deployable composite thin-walled lenticular tubes[J]. Composite Structures, 2016, 153: 601-613.
[12] [12] HU M Y, WANG A W. Free vibration and stresses analysis of fiber-reinforced viscoelastic composite laminated plates[J]. Engineering Mechanics, 2010, 27(8): 10-14, 20.(in Chinese)
HU M Y, WANG A W. Free vibration and stresses analysis of fiber-reinforced viscoelastic composite laminated plates[J]. Engineering Mechanics, 2010, 27(8): 10-14, 20.(in Chinese)
[13] [13] FANG G Q, PENG F J. Fabrication and retraction/deployment testings of space deployable booms[J]. Journal of Materials Engineering, 2009, 37(S2): 157-160.(in Chinese)
FANG G Q, PENG F J. Fabrication and retraction/deployment testings of space deployable booms[J]. Journal of Materials Engineering, 2009, 37(S2): 157-160.(in Chinese)
[14] [14] BORDOGNA M T, MACQUART T, BETTEBGHOR D, et al.. Aeroelastic optimization of variable stiffness composite wing with blending constraints[C].17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Washington, D.C.. Reston, Virginia: AIAA, 2016.
BORDOGNA M T, MACQUART T, BETTEBGHOR D, et al.. Aeroelastic optimization of variable stiffness composite wing with blending constraints[C].17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Washington, D.C.. Reston, Virginia: AIAA, 2016.
[15] [15] AGARWAL G, PATNAIK A, SHARMA R K, et al.. Effect of stacking sequence on physical, mechanical and tribological properties of glass-carbon hybrid composites[J]. Friction, 2014, 2(4): 354-364.
AGARWAL G, PATNAIK A, SHARMA R K, et al.. Effect of stacking sequence on physical, mechanical and tribological properties of glass-carbon hybrid composites[J]. Friction, 2014, 2(4): 354-364.
[16] [16] EHSANI A, REZAEEPAZHAND J. Stacking sequence optimization of laminated composite grid plates for maximum buckling load using genetic algorithm[J]. International Journal of Mechanical Sciences, 2016, 119: 97-106.
EHSANI A, REZAEEPAZHAND J. Stacking sequence optimization of laminated composite grid plates for maximum buckling load using genetic algorithm[J]. International Journal of Mechanical Sciences, 2016, 119: 97-106.
[17] [17] GONG K. The Effect of Stacking Sequence on Impact Resistance and Damage Tolerance in Non-crimp Carbon Fabric Composites[D]. Manchester: The University of Manchester,2015.
GONG K. The Effect of Stacking Sequence on Impact Resistance and Damage Tolerance in Non-crimp Carbon Fabric Composites[D]. Manchester: The University of Manchester,2015.
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YANG Hui, FAN Shuo-shuo, LIU Rong-qiang. Optimization of single lenticular honeycomb boom for optical film deployable mechanism[J]. Optics and Precision Engineering, 2020, 28(10): 2244
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Received: Feb. 25, 2020
Accepted: --
Published Online: Nov. 25, 2020
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