Advanced NACA 4412 Airfoil Analysis ( by implementing synthetic jet )
Budget: $30 – $250 USD
I need an analysis of a NACA 4412 airfoil by implementing synthetic jet using ANSYS. The outcomes should capture:
- Accurate lift and drag coefficients
- Pressure distribution
- Mesh sizing
.The assessment needs to be conducted under 30 m/s flow speed. Lift, drag coefficients should be calculated at different angle of attacks (0 and 15 degree) The right freelancer will have extensive experience with aerodynamics, NACA airfoils, and proficiency in ANSYS. Deep understanding of flow control is a must.
- Accurate lift and drag coefficients
- Pressure distribution
- Mesh sizing
.The assessment needs to be conducted under 30 m/s flow speed. Lift, drag coefficients should be calculated at different angle of attacks (0 and 15 degree) The right freelancer will have extensive experience with aerodynamics, NACA airfoils, and proficiency in ANSYS. Deep understanding of flow control is a must.