Time Domain Boundary Element Method Prediction of Noise Shielding by a NACA 0012 Airfoil
AIAA AVIATION 2021 FORUM
2021-01-01
Conference paper
Electronic Resource
English
Experimental Study of Noise Shielding by a NACA 0012 Airfoil (AIAA 2018-2821)
British Library Conference Proceedings | 2018
|