01271nam a2200265 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245017100119300003000290545007400320545004300394545009500437653019700532700004100729700001400770700001100784773014000795856002000935900001800955900002000973900001200993KSI00009872620040203234715031201s2001    ulka          000   kor    a0110010 akorbeng01a558.05b한642c29(7)00a공압식 구동장치가 부착된 조종날개의 공력탄성학적 특성=xAeroelasticity of control fin with pneumatic actuator/d배재성,e백승길,e이인  ap. 27-33:b삽도;c26 cm  a배재성, 정회원, 한국과학기술원 항공우주공학 전공  a백승길, 한국항공우주산업㈜  a이인, 정회원, 한국과학기술원 항공우주공학 전공binlee@asdl.kaist.ac.kr  a공압식 구동장치a조종날개?a공력탄성학aAeroelasticityaControlaFinaPneumatic actuatoraFluttera플러터aFictitious mass methoda가상질량법aNonlinearitya비선형성1 a배재성,d1972-0KAC2018498074aut1 a백승길1 a이인0 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g29卷 7號(2001년 10월), p. 27-33q29:7<27w(011001)KSE199509707,x1225-134840u3328187aKd00010aBae, Jae-Sung10aPaek, Seung-Kil10aLee, In