Experimental Investigation to Study Flow Characteristics over a Naca0018 Aerofoil and an Automobile Dome-A Comparative Study
نویسندگان
چکیده
Experiments are carried out to study static pressure distribution and drag variations over NACA0018 aerofoil and over an automobile dome. Static pressure coefficients are calculated along the chord length for different angles of attack for both the test models and the results are compared. Further, the relationship between coefficient of drag and Reynolds number has been arrived for different angles of incidence. It was found that coefficient of drag decreases as the Reynolds number increases and cd is higher at higher angles of incidence for both the aerofoil and automobile dome.
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