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Aerodynamics at low speeds has an increasing interest for engineers due to new concepts of drones and urban mobility aircraft. An important physical phenomenon called Laminar Separation Bubble may impact the performance and safety of such machines. In this work we propose a new model that predicts this phenomenon using modern Computational Fluid Dynamics simulations.

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This page is a summary of: Algebraic Nonlocal Transition Modeling of Laminar Separation Bubbles Using k−ω Turbulence Models, AIAA Journal, February 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j057734.
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