Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method
The aeronautical journal ; 110 , 1111
2006
Aufsatz (Zeitschrift)
Unbekannt
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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