OPTIMIZATION DESIGN OF HELICOPTER FOR PRELIMINARY PARAMETERS

作     者：Guo Caigen (The Research Institute of Helicopter Technology, Nanjing University of Aeronautics and Astronautics, Nanjing China 210016) 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：1994年第7卷第3期

页      面：175-182页

核心收录：

学科分类：08[工学] 082503[工学-航空宇航制造工程] 0825[工学-航空宇航科学与技术] 

主　　题：helicopters optimization design computer aided design 

摘      要：A new design method for prehminary parameters is proposed. The analyticmodels of the optimization design are established according to the requirements of helicopter flight performance- stability, engine and weight. The optinial preliminary projectof design to meet the requirements of critenon for helicopter design is worked out byapplying the computer and optimization techniques. The inethod can be used for theanalysis of helicopters for prehminary parameters that are used in practice and for theanalysis of sensibility for preliminary parameters, too. The method is shown to be veryuseful by the example and application in the new design of helicopters.