A Hybrid Blade Element Momentum Model for Flight Simulation of Rotary Wing Unmanned Aerial Vehicles. Davoudi, B & Duraisamy, K In AIAA Aviation Forum, pages 1–21, Dallas, Texas, 2019.
doi  bibtex   
@InProceedings{Davoudi2019,
    author      = {Davoudi, B and Duraisamy, K},
    title       = {A Hybrid Blade Element Momentum Model for Flight Simulation of Rotary Wing Unmanned Aerial Vehicles},
    address     = {Dallas, Texas},
    booktitle   = {{AIAA} Aviation Forum},
    doi         = {10.2514/6.2019-2823},
    pages       = {1--21},
    year        = {2019}
}

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