Results of studying the aerodynamic performance for a multipurpose medium lift helicopter model are presented. Both integrated and distributed aerodynamic performance of the model is presented along with flow distribution characteristics in the vicinity of the fuselage. The influence of two different rear fuselage geometries on the aerodynamic performance of the fuselage is discussed.
Investigation of Aerodynamic Performance of a Multipurpose Medium Lift Helicopter with Different Rear Fuselage Geometries
Russ. Aeronaut.
Russian Aeronautics ; 64 , 2 ; 248-255
2021-04-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aerodynamic Investigations on a Helicopter Fuselage
AIAA | 2011
|Aerodynamic Drag Prediction of Helicopter Fuselage
AIAA | 2001
|Aerodynamic Analysis of a Helicopter Fuselage
Tema Archiv | 2010
|Aerodynamic Investigations on a Helicopter Fuselage
British Library Conference Proceedings | 2011
|