01526nam a2200217 c 4500001001300000005001500013008004100028041001300069049003200082052002100114056001600135082001800151100004800169245021700217260003600434300003200470502008600502590003000588653066600618900002401284KDM20042567020040626103150040318s2003    ulkaf      AK 000   eng  0 aengbkor0 lWM402398lWM402399c複fDP02a629.13432bG491m  a558.3432240 a629.134322211 a김유신,g金庾信,d1972-0KAC20184689200aMultidisciplinary multi-point design optimization of supersonic fighter wing using response surface methodology=x반응면 기법을 이용한 초음속 전투기 날개의 다학제간 다점 설계/d김유신  a서울:b서울대학교,c2003  axiii, 123p.:b삽도;c26cm1 a학위논문(박사) --b서울대학교 대학원:c항공우주공학과,d2003  y열람용은 복사본임  aMULTIDISCIPLINARY DESIGN OPTIMIZATIONaSUPERSONIC FIGHTER WINGaRESPONSE SURFACE METHODOLOGYaAEROELASTIC ANALYSISaSINGLE-POINT DESIGNaMULTIPOINT DESIGNaWEIGHTED SUM METHODaFEASIBILITY OF DESIGN SPACEaPROBABILISTIC APPROACHaPROBABILITY DENSITY FUNCTIONaCUMULATIVE DISTRIBUTION FUNCTIONaJOINT PROBABILITY THEORYaMONTE-CARLO SIMULATIONaGENETIC ALGORITHMa반응면 기법a초음속 전투기 날개a전투기 날개a다학제간 최적설계a항공우주공학a공탄성 해석a단일점 설계a다점설계a가중치기법a설계공간 타당성a확률론적 해석기법a확률이론a몬테카를로 시뮬레이션a유전적 알고리즘10aKim, Yushin,d1972-