Adjoint-Based Aerodynamic Optimization of Supersonic Biplane Airfoils
نویسندگان
چکیده
منابع مشابه
Adjoint-Based Aerodynamic Optimization of Supersonic Biplane Airfoils
This paper addresses the aerodynamic performance of Busemann-type supersonic biplanes at both design and offdesign conditions. An adjoint-based optimization technique is used to optimize the aerodynamic shape of the biplane to reduce the wave drag at a series of Mach numbers ranging from 1.1 to 1.7, at both acceleration and deceleration conditions. The optimized biplane airfoils dramatically re...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2012
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.c031417