作者: N. Qin , A. Vavalle , A. Le Moigne , M. Laban , K. Hackett
DOI: 10.1016/J.PAEROSCI.2004.08.001
关键词: Wing 、 Viscous flow 、 Panel method 、 Aerodynamics 、 Engineering 、 Aerospace engineering 、 Design studies 、 Performance improvement 、 Planform 、 Airfoil
摘要: In this paper, we present a progressive aerodynamic study of a blended wing body (BWB) configuration within a European project, MOB (A computational design engine incorporating …