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- W2620794119 endingPage "012080" @default.
- W2620794119 startingPage "012080" @default.
- W2620794119 abstract "The Aircraft wing is a point of important research which poses greater challenge in terms of aerodynamic efficiency. The flow separation control method is addressed in classical aerodynamics methods. This study focuses on influence of dimples on controlling the flow and also increasing the aerodynamic efficiency. The periodic process of placing the cavities on the wing starting from root to tip controls the flow separation. The linear variation of characteristic curve provides the information about the flow separation and control of flow on upper surface of the airfoil.These different shapes are utilized viz., Square, Rectangle and Triangle. The numerical simulation is carried out in using MATLAB package. Preliminary analysis on the flow separation is carried out focuses on laminar flow separation, which has the influence on the overall lift generation and drag generation." @default.
- W2620794119 created "2017-06-09" @default.
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- W2620794119 date "2017-05-01" @default.
- W2620794119 modified "2023-09-26" @default.
- W2620794119 title "Numerical simulation of dimples in airfoil using MATLAB" @default.
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- W2620794119 doi "https://doi.org/10.1088/1757-899x/197/1/012080" @default.
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