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首页> 外文期刊>Russian Aeronautics >Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing
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Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing

机译：Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing

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摘要

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.

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