To determine the aerodynamic loads on the structural elements of the mobile-deployable landing platform, numerical modeling of the turbulent flow of a viscous compressible gas induced by the rotation of the helicopter rotor is carried out. The flowfield around the helicopter is determined on the basis of numerical calculations, and the pressure distribution on the structural elements of the landing platform is discussed.
Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing
Russ. Aeronaut.
Russian Aeronautics ; 65 , 2 ; 297-305
2022-04-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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