Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps
45th AIAA Aerospace Sciences Meeting and Exhibit
2007-01-01
Conference paper
Electronic Resource
English
Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
Online Contents | 2007
|Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps AIAA Paper
British Library Conference Proceedings | 2007
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