Abstract
Based on structure dynamics finite element method (FEM) numerical analysis, and optimal design methods, this paper analyzed the finite element modeling of cabin structure of nose landing gear and discussed optimal design of structural parameter. The main research work conducted included the following: Finite element discretization of structure of nose landing gear, construction of finite element model, optimal variable design, optimal design for component dimension parameter of structural low-order frequency property in numerical value technique frame, lightest structural weight under low-order frequency restriction conditions, and best geometrical stiffness structure distributing. The thesis introduced in details the structure dynamic characteristic finite element mesh adopted in performance calculation as well as the structure numerical optimal theory and discussed every detail of optical design for numerical value of intrinsic dynamic characteristics and the optimal analysis results. At the end of the paper, the author proposes the conclusion of the research.
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References
Walker N, Philbin DA, Fisk AD (1997) Age-related differences in movement control: adjusting submovement structure to optimize performance. J Gerontol Ser B: Psychol Sci Soc Sci 52:40–53
Pu X, Liu X, Qiu F et al (2004) Novel method to optimize the structure of reticulated porous ceramics. J Am Ceram Soc 87:1392–1394
Chu DN, Xie YM, Hira A et al (1996) Evolutionary structural optimization for problems with stiffness constraints. Finite Elem Anal Des 21:239–251
Xie YM, Steven GP (1997) Basic evolutionary structural optimization. Springer, London
Fleury C, Braibant V (1986) Structural optimization: a new dual method using mixed variables. Int J Numer Meth Eng 23:409–428
Fadel GM, Riley MF, Barthelemy JM (1990) Two point exponential approximation method for structural optimization. Struct Optim 2:117–124
Ha SK, Keilers C, Chang FK (1992) Finite element analysis of composite structures containing distributed piezoceramic sensors and actuators. AIAA J 30:772–780
Svanberg K (1987) The method of moving asymptotes—a new method for structural optimization. Int J Numer Meth Eng 24:359–373
Xie YM, Steven GP (1993) A simple evolutionary procedure for structural optimization. Comput Struct 49:885–896
Toropov VV (1989) Simulation approach to structural optimization. Struct Optim 1:37–46
Barthelemy JF, Haftka RT (1993) Approximation concepts for optimum structural design—a review. Struct Optim 5:129–144
Hale AL, Dahl WE, Lisowski J (1985) Optimal simultaneous structural and control design of maneuvering flexible spacecraft. J Guidance Control Dyn 8:86–93
Kicinger R, Arciszewski T, Jong KD (2005) Evolutionary computation and structural design: a survey of the state-of-the-art. Comput Struct 83:1943–1978
Perez RE, Behdinan K (2007) Particle swarm approach for structural design optimization. Comput Struct 85:1579–1588
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Tian, W., Sun, Q. (2014). Applied Design Optimization of Nose Landing Gear Cabin Structure of Airplane. In: Wang, J. (eds) Proceedings of the First Symposium on Aviation Maintenance and Management-Volume II. Lecture Notes in Electrical Engineering, vol 297. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-54233-6_61
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DOI: https://doi.org/10.1007/978-3-642-54233-6_61
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