Automatic airfoil and wing design based on dynamic modeling of structural and aerodynamic performance

Systems, methods, and non-transitory computer-readable media are disclosed for automatically generating an improved aircraft wing by modifying quantitative design variables of one or more airfoils based on joint analysis of aerodynamic and structural performance. In particular, the disclosed systems...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Roberts, Nicholas, Colas, Dorian Frederic Marie, Suryakumar, Vishvas Samuel
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING HELICOPTERS PERFORMING OPERATIONS PHYSICS TRANSPORTING
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