01346nam a2200265 c 4500001001300000005001500013008004100028040001100069041001300080052003300093245027600126300002200402545007000424545005400494545005400548653013700602700004100739700004800780700003600828773014400864856002101008900001701029900001601046900001801062KSI00056574920060830134622060825s2003    ulk           000   kor    a0110010 akorbeng01a558.05b한642c31(6)-31(10)00a초음속 충동형 터빈익형의 공력성능 향상을 위한 기하학적 설계변수 수치연구=xNumerical investigation of geometrical design variables for improvement of aerodynamic performance of supersonic impulse turbine/d이은석,e김진한,e조광래  ap. 99-106;c26 cm  a이은석, 정회원, 한국항공우주연구원besl@kari.re.kr  a김진한, 정회원, 한국항공우주연구원  a조광래, 정회원, 한국항공우주연구원  aTurbopumpa터보펌프aPartial admissiona부분흡입형aImpulse turbinea충동형터빈aAerodynamic redesigna공력재설계1 a이은석,d1966-0KAC2018558884aut1 a김진한,g金鎭漢,d1963-0KAC2018384601 a조광래,d1959-0KAC2018494920 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g제31권 8호(2003년 10월), p. 99-106q31:8<99w(011001)KSE199509707,x1225-134840u40132983aKd00010aLee, Eunseok10aKim, Jinhan10aCho, Gwangrae