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황재업,배재성,황재혁,홍예선,박상준,정태경,Hwang, Jaeup,Bae, Jaesung,Hwang, Jaihyuk,Hong, Yehsun,Park, Sangjoon,Chung, Taekyong 항공우주시스템공학회 2014 항공우주시스템공학회지 Vol.8 No.1
This thesis is simulated a aircraft nose landing gear drop-test. flow rate-to-pressure difference characteristics of damping orifices for a nose landing gear is investigated by CFD analyses. Orifice is kind of poppet valve type. it is simulated pressure drop with variable orifice area. it is simulated landing gear model by using ADAMS with CFD result. It's performance evaluated landing gear drop-test and analyzed the results.