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@article{169058,
        author = {JAGADEESH.Y.J},
        title = {Flow study by Simulation over Drone-Aerofoil blade},
        journal = {International Journal of Innovative Research in Technology},
        year = {2024},
        volume = {11},
        number = {6},
        pages = {252-254},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=169058},
        abstract = {Flow study with Incompressible flow  simulation  is done for the drone aerofoil blade with few angle of attack. The blades are  similar to NACA types of blades. Pattern of Flow pattern with distribution of surface pressure are studied. The stagnation point is noted.  Discretization of the governing equations by control volume is used. Fluent Software is used to get the result.},
        keywords = {Angle, Control Volume, Drone blade, Fluent, simulation, surface pressure},
        month = {November},
        }