01415naa a2200265 c 4500001001300000005001500013008004100028040001100069041001300080052002600093245026800119300002700387545008200414545008200496545008200578546002500660653016800685700004800853700001400901700003600915773014200951900001901093900001801112900001901130KSI00096258320200702132444200629s2020    ulk           000   kor    a0110010 akorbeng01a558.05b한642c48(2)00a3차원 patched-grid 알고리즘을 이용한 삼각 날개–원통형 동체 형상 전산 해석 =xComputational analysis of the delta wing-cylindrical body configuration using the three-dimensional patched-grid algorithm /d박현돈,e김영진,e박수형  ap. 109-117 ;c26-28 cm  a박현돈, Department of Aerospace Information Engineering, Konkuk University  a김영진, Department of Aerospace Information Engineering, Konkuk University  a박수형, Department of Aerospace Information Engineering, Konkuk University  a영어 요약 있음  a전산유체역학aEFD-CFD 워크숍a삼각익a접합 격자계 알고리즘aComputational fluid dynamicsaEFD-CFD workshopaDelta wingaPatched-grid algorithm1 a박현돈,g朴鉉暾,d1995-0KAC2021N92851 a김영진1 a박수형,d1973-0KAC2017180140 t韓國航空宇宙學會誌.d韓國航空宇宙學會.g48권 2호(2020년 2월), p. 109-117q48:2<109w(011001)KSE199509707,x1225-134810aPark, Hyeondon10aKim, Youngjin10aPark, Soohyung