1135-1205 Aerodynamic Optimization of Supersonic Wing-Nacelle Configuration Using an Adjoint Method with the Unstructured-Grid Approach
International workshop; 2nd, Numerical simulation technology for design of next generation supersonic civil transport ; 2000 ; Tokyo
2000-01-01
10 pages
Conference paper
English
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Aerodynamic optimization of supersonic transport wing using unstructured adjoint method
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