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IMPROVED LANDING-GEAR DESIGN FOR FLEXIBLE AIRPLANE
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作者 史友进 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2005年第3期224-229,共6页
Landing dynamic simulation and landing-gear optimization design are used to improve the landing-gear design for a flexible airplane. Landing response is simulated by using velocity-squared damping, polytropic exponent... Landing dynamic simulation and landing-gear optimization design are used to improve the landing-gear design for a flexible airplane. Landing response is simulated by using velocity-squared damping, polytropic exponential air-compression spring, tire force power function characteristics, and an equivalent three-mass system.Optimization of landing-gear parameters is performed considering the maximum displacement of the landing-gear shock stroke, the maximum landing-gear force and the maximum deformation of the wingtip in the landing impact. Resutls show that landing-gear design parameters have an important influence on the structural flexibility of the airplane. And the landing performance of the landing-gear can be improved by the optimized metering pin type landing-gear. 展开更多
关键词 flexible airplane landing response dynamic simulation landing-gear optimization design passive control
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