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NLF Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction
NLF Airfoil Wing Design Adjoint Method Automatic Transition Prediction
2015/7/3
This paper describes the application of optimization technique based on control theory for natural-laminar-°ow airfoil and wing design in viscous compressible °ow modeled by the Reynolds averaged Navi...
Challenges and Complexity of Aerodynamic Wing Design
Challenges Complexity Aerodynamic Wing Design
2015/7/2
This paper focuses on aerodynamic design methodology. It discusses challenges and complexity of aerodynamic wing design for a transonic aircraft, which arise from the complex nature of ow around the w...
While aerodynamic prediction methods based CFD are now well estab lished, and quite accurate and robust, the ultimate need in the design process is to find the optimum shape which maximizes the ...
Paul Garabedian's Contributions to Transonic Airfoil and Wing Design
Transonic Airfoil Wing Design
2015/6/23
This note on Paul Garabedian's work on transonic airfoil and wing
design is written from the perspective of aeronautical engineering as well
as applied mathematics. Paul's contributions in this area...
Aspects of Wing Design
Wing Design plane
2015/6/18
Another key issue for successful implementation of the continuous adjoint
method is the choice of an appropriate inner product for the definition of the
gradient. It turns out that there is an...