Convolution Kernels for a NACA 0012 Airfoil Based on Unsteady Pressure Wind Tunnel Measurements
AIAA SCITECH 2024 Forum
2024-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Investigation of NACA 0012 Airfoil Periodic Flows in a Transonic Wind Tunnel
British Library Conference Proceedings | 2013
|Numerical Simulation of a Pitching NACA 0012 Airfoil
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