CFD & XFLR5 Analysis on NACA23015 Airfoil

I am looking for a professional with expertise in Computational Fluid Dynamics (CFD) and XFLR5 to conduct a comprehensive flow analysis on the NACA23015 airfoil for the A320neo design. This analysis should cover both laminar and turbulent conditions, as well as all flight scenarios including takeoff, cruise and landing. Create reasonable assumptions for the CFD simulation as well as the enclosure and locations of the inlet, outlet and walls. The flow analysis has to analyze three sections of the wing, middle (fuselage) of the wing, the middle, and the wingtip section.

When done with the XFLR5 - provide hand calculations for validation of the flow analysis results too.

Key Analysis Parameters:
- Lift coefficient (Cl)
- Drag coefficient (Cd)
- Pressure distribution
- Drag
- Lift
- Contour of static pressure
- Velocity magnitude

Ideal candidates should have a strong background in aerodynamics and experience with airfoil modeling. Proficiency in using CFD and XFLR5 software is a must, as well as the ability to interpret and present complex data in a clear and concise manner.