What is it about?

A helicopter rotor produces a downward force to maintain a hover, however it also creates a complex wake system that interacts with the fuselage and ground that produces upward forces on the rotor blades and fuselage. This paper uses high-fidelity computational simulations to quantify these force components and show how the forces are highly dependent on the positions of the rotor blades as they rotate.

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Why is it important?

Our findings show that the chosen computational approach can accurately replicate the test results at several different flight conditions. Additionally, we quantify the benefit of hovering close to the ground and the efficiency losses associated with the fuselage and a headwind.

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This page is a summary of: Isolated and Installed Rotor Simulations of a Scaled Helicopter Rotor in Hover Using Wall-Modeled Large-Eddy Simulation, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2024-0897.
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