Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
Russian aeronautics ; 59 , 1
2016
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik | |
Lokalklassifikation TIB: | 770/7040/8000 |
Approximate technique of tip vortex account in calculating a helicopter main rotor
Online Contents | 2012
|Approximate technique of tip vortex account in calculating a helicopter main rotor
Springer Verlag | 2012
|Calculating Flow Through A Helicopter Rotor
NTRS | 1991
|Vortex flow over helicopter rotor tips
AIAA | 1971
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