Aerodynamics of High-Subsonic Blended-Wing （空气动力学的High-Subsonic审视）.pdf
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41st Aerospace Sciences Meeting and Exhibit AIAA 2003-554
6-9 January 2003, Reno, Nevada
AERODYNAMICS OF HIGH-SUBSONIC
BLENDED-WING-BODY CONFIGURATIONS
Dino Roman* Richard Gilmore† Sean Wakayama‡
The Boeing Company The Boeing Company The Boeing Company
Huntington Beach, CA 92647 Huntington Beach, CA 92647 Huntington Beach, CA 92647
Abstract
A Mach 0.93 Blended-Wing-Body (BWB) 1.2 BWB
configuration was developed using CFL3DV6, a Sears-Haack
a
e
Navier-Stokes computational fluid dynamics (CFD) r 1.0
A
l MD-11
code, in conjunction with the Wing Multidisciplinary a
n
o
i
Optimization Design (WingMOD) code, to
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