7. Make a literature search and state clearly and briefly what you understand from Kutta condition and its use in aerodynamics.
- Kutta condition is a principle in steady - flow dynamics, i.e aerodynamics, which is applicable to solid bodies with sharp corners, such as tariling edges of airfoils.
- Kutta condition allows an aerodynamicst to incorporate a significant effect of viscosity while neglecting vicous effect in the underlying conservation of momentrum equation. It is important in the practicle calculation of list on a wing.
- Mathematically, the kutta condition enforces a specific choice among the infinite allowed values od circulation.
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