The propulsive airfoil is investigated by determining the optimum air flow rate taken from the surface and comparing it with the air flow rate of the engines installed on the helicopter. The lift force generated by the developed airfoil is compared with the helicopter launch weight.
Study of Aerodynamics of Propulsive Helicopter Fuselage
Russ. Aeronaut.
Russian Aeronautics ; 66 , 3 ; 493-499
01.08.2023
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Computation of Helicopter Fuselage Aerodynamics Using Navier-Stokes CFD Methods,
Online Contents | 2000
|Helicopter fuselage aerodynamics under a rotor by navier-stokes simulation
Online Contents | 1997
|Computation of helicopter fuselage aerodynamics using Navier-Stokes CFD methods
Tema Archiv | 2000
|Sliding Mesh Algorithm for CFD Analysis of Helicopter Rotor-Fuselage Aerodynamics
British Library Conference Proceedings | 2008
|Sliding mesh algorithm for CFD analysis of helicopter rotor-fuselage aerodynamics
Tema Archiv | 2008
|