Modelling of airfoil-vortex interaction and application to a helicopter rotor. Contribution to blade-vortex interaction noise prediction
Modélisation de l'interaction profil-tourbillon et application au rotor d'hélicoptère. Contribution à la prévision du bruit d'interaction pale-tourbillon
1998
212 S
Translated from ONERA-PB 97-02
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Theses
English
BKL: | 55.50 Luftfahrzeugtechnik |
Rotor blade-vortex interaction noise
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