Time Domain Boundary Element Method Prediction of Noise Shielding by a NACA 0012 Airfoil
AIAA AVIATION 2021 FORUM
2021-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Experimental Study of Noise Shielding by a NACA 0012 Airfoil (AIAA 2018-2821)
British Library Conference Proceedings | 2018
|Dynamic stall experiments on the NACA 0012 airfoil
TIBKAT | 1978
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