An unsteady Reynolds-averaged Navier-Stokes solver for unstructured grids is used to compute the rotor airloads on the UH-60A helicopter at high-speed and high thrust conditions. The flow solver is coupled to a rotorcraft comprehensive code in order to account for trim and aeroelastic deflections. Simulations are performed both with and without the fuselage, and the effects of grid resolution, temporal resolution and turbulence model are examined. Computed airloads are compared to flight data.
Computation of UH-60A Airloads Using CFD/CSD Coupling on Unstructured Meshes
American Helicopter Society 67th Annual Forum and Technology Display ; 2011 ; Virginia Beach, VA, United States
2011-05-03
Aufsatz (Konferenz)
Keine Angabe
Englisch
Computation of UH-60A Airloads Using CFD/CSD Coupling on Unstructured Meshes
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