25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-P2.16
AERODYNAMIC DESIGN FOR WING-BODY BLENDED AND INLET
Q. Z. Yang, Y. Zheng, T. Streit*
Northwestern Polytechnical Univ., China; *DLR, Germany
Keywords: Aerodynamic, Design, Blended Wing-Body, Inlet
A wing-body blended configuration for transport and the other two for unmanned air vehicle are designed using box complex search approach optimization method and inverse design method. The twists of wing section are optimized using composite method, and the airfoils on wing sections are designed using iterative residual correction method.
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