Thermal and aerodynamic performances of the supersonic motion
نویسندگان
چکیده
منابع مشابه
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چکیده ندارد.
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: Thermal Science
سال: 2010
ISSN: 0354-9836
DOI: 10.2298/tsci100222011n