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고강명(KangMyung Ko),강승온(SeungOn Kang),김상훈(SangHun Kim),이동호(DongHo Lee),장용진(YongJin Chang),최원(Won Choi),황유상(YuSang Hwang),김철호(CheolHo Kim) 대한기계학회 2007 대한기계학회 춘추학술대회 Vol.2007 No.5
It is necessary a simple helicopter design and performance analysis program for a stage of helicopter conceptual design. To meet that needs, we have developed a program which is simply used to estimate helicopter configuration and performance. The program developed by this study is composed of Requirement, Mission profile Analysis, Size, Aerodynamic, Trim, Propulsion, Weight, and Performance modules, and each modules carry out operations for a given flight condition. In this study, we validate this analysis program in 9,500 lbs and 22,000 lbs helicopters and estimate design configuration and performance of 16,000 lb helicopter. And We can use this program to optimization process for Helicopter MDO framework.