3Kimiey D J,Halm A S,Gelhauseii P A.Comparison of low and high nacelle subsonic transport configurations.AIAA paper,1997:97-2318.
4Fujino M,Kawamura Y,Wave-drag characteristics of an over-the-wing nacelle business-jet configuration.Journal of Aircraft,2003;40(6):1177-1184.
5Hill G A,Kandil O A,Hahn A S.Aerodynamic investigations of an advanced over-the-wing nacelle transport aircraft configuration,Journal of Aircraft,2009;46(1):25-35.
7Aftosmis M J,Berger M J,Alonso J J.Applications of a cartesian mesh boundary-layer approach for complex configurations.AIAA Paper,2006:2006-0652.
8Epstein R J,Carbonaro M C,Caudron F.Experimental investigation of the flow field about an upswept afterbody[J].Journal of Aircraft,1994,31(6):1281-1290.
9Haar D,Brezillon J.Engine integration based on multidisciplinary optimization technique[J].CEAS AeronauticalJournal,2012,3(1):17-24.
10Smith R E.Transfinite interpolation (TFI) generation systems[M].Handbook of Grid Generation.Cleveland:CRC Press,1998.