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In this project steady state incompressible fluid flow simulation of a small RC aircraft is performed for the completion of aircraft design course on SimScale's Academy. Two simulation at different AOA relative to wing is carried out to obtain the coefficient of lift and drag. Lift and drag forces are calculated at 3 and 20 AOA, also the flow around the aircraft is also visualized for the design consideration.

Cessna 208 Caravan Airfoil - CFD Simulation
- develop a more concrete understating of the air flow around the planes wing in a realistic scenario (approx. 80mph air speed)

This  Study, investigates the possibility and the benefits of using a cross-flow fan embedded in an airfoil for simultaneous circulation control and thrust generation. In the propulsive wing concept, a cross flow fan is placed near the trailing edge of an airfoil section. When the fan starts to operate, the flow is drawn from the suction surface, provided by energy through the cross-flow fan and expelled out of the airfoil trailing edge

Aircraft simulation  lift ,drag,thrust checking in all angles

NACA2408 Aerofoil Spoiler Basic CFD Analysis

CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees.

Reference:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf

* 3D Airfoil Simulation with AOA.
* Level 1 and 2 assignments

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