High-Order Implicit Shock Tracking for a Supersonic Biplane Airfoil
AIAA AVIATION 2022 Forum
01.01.2022
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Investigation of Supersonic Wing Shape Using Busemann Biplane Airfoil AIAA Paper
British Library Conference Proceedings | 2007
|Online Contents | 2011
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