The calculation of a hydrodynamic profile for a fluid that flows around mainly consists in de-termining the variation of drag force and lift force. Thus, for NACA 6412 profile, we will calculate and com-pare the changes of values of the coefficient forces mentioned above. The calculation will be done both experimentally in a naval wind tunnel and with a computational fluid dynamics - CFD (ANSYS 13). These experimental and numerical approaches can be used to study finite scale naval profiles such as the rudder.
Nowadays, there can be observed a need to understand the mechanisms offeree generation by flapping wings in a more comprehensive way. The paper offers a summary, based on the-state-of-the-art in aerospace engineering and biological literature. The main purpose of the paper is to integrate both of them in the hope of constructing a more synthetic view of force generation in a flapping flight.
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