01254nam a2200265 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245023100119300003000350545003700380545005300417545005300470653017200523700001900695700004800714700001400762773013400776856002000910900002000930900001800950900002000968KSI00009335920040213234445031127s1992    ulka          000   kor    a0110010 akorbeng01a558.05b한642c20(1)00a정지 비행시 헬리콥터 회전날개의 공력탄성학적 안정성에 대한 유한요소해석=xFinite element analysis for aeroelastic stability of helicopter rotor blade in hover/d신상준,e정성남,e김승조  ap. 45-54:b삽도;c26 cm  a신상준, 국방과학연구소  a정성남, 서울대학교 항공우주공학과  a김승조, 서울대학교 항공우주공학과  a정지비행a헬리콥터a회전날개a공력탄성학a안정성a유한요소해석aFinite element analysisaAeroelastic stabilityaHelicopter rotor bladeaHover1 a신상준4aut1 a정성남,g鄭城男,d1963-0KAC2017074311 a김승조0 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g20권 2호(1992. 6), p. 45-54q20:2<45w(011001)KSE199509707,x1225-134840u3326099aKd00010aChung, Sung-Nam10aKim, Seung-Jo10aShin, Sang-Joon