WIND TUNNEL TEST OF OPTIMAL ROTOR BLADE TIP FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO
The @Vertical Flight Society ; 77. ; 2021 ; Online
2021
Aufsatz (Konferenz)
Englisch
OPTIMAL DESIGN OF ROTOR BLADE FOR A WINGED COMPOUND HELICOPTER AT HIGH ADVANCE RATIO
British Library Conference Proceedings | 2020
|