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Hover performance prediction is important for design of helicopter rotors. This work presents a steady-state CFD method that delivers accurate results for a wide range of blade planform shapes. The predictions are compared against test data and detailed validation is presented.
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This page is a summary of: Validation of the Steady-State Hover Formulation for Accurate Performance Predictions, AIAA Journal, December 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058408.
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