Adjoint quasi-three-dimensional aerodynamic solver for multi-fidelity wing aerodynamic shape optimization

Journal article (2015)

Authors

A. Elham Flight Performance and Propulsion - Aerospace Engineering
Research Group
Flight Performance and Propulsion (Aerospace Engineering) (TU Delft)
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Published Date

2015

Language

English

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Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Flight Performance and Propulsion