Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
31st AIAA Applied Aerodynamics Conference
2013-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
British Library Conference Proceedings | 2013
|Adjoint-based Method for Supersonic Aircraft Design Using Equivalent Area Distribution
British Library Conference Proceedings | 2012
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