Adjoint-Based Optimisation of a Blended Wing Body Aircraft with Shock Control Bumps AIAA Paper
45th, AIAA aerospace sciences meeting ; 2007 ; Reno, NV
2007-01-01
2007-57-2007-836
Papers in the range 2007 17 to 1467 with gaps. Held on CD-ROM
Conference paper
English
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Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
Online Contents | 2007
|AIAA-2002-5448 Aerodynamic Studies for Blended Wing Body Aircraft
British Library Conference Proceedings | 2002
|British Library Conference Proceedings | 2007
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