Then perform CFD simulation using the Acusolve software. Then from that calculate lift force, drag force and lift coefficient. Perform wind tunnel analysis and record pressure head at different points by varying angle of attack and wind velocity in succession. You can learn from experts, build working projects, showcase skills to the world and grab the best jobs. You can enrol with friends and receive kits at your doorstep Skyfi Labs helps students learn practical skills by building real-world projects. It produces a fairly accurate result with ease and convenience. CFD: Computational Fluid Dynamics (CFD) is the science of predicting fluid flow, heat and mass transfer, chemical reactions, and related phenomena using numerical methods. The shape of the NACA airfoils is described using a series of digits following the word "NACA”. NACA Airfoil: The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). This can be seen in the cross-section of wings, propeller blades, windmill blades, compressor, and turbine blades in a jet engine. Airfoil: An airfoil is a body of such a shape that when it is placed in an airstream, it produces an aerodynamic force. Compare both the result to validate your CFD result. 
Then perform CFD simulation using Acusolve to find out a numerical solution. Perform Wind tunnel analysis to get experiment result data regarding lift, drag and stall with respect to the various angle of attack at various airspeed. Make a scaled model prototype of standard NACA airfoil for both wind tunnel analysis and CFD simulation purpose. At 1st you have to apply the basic physical laws of engineering and science to understand the principles of flight. so, you need to choose a standard NACA 4-digit series symmetrical airfoil for this project. A symmetrical airfoil better suits for frequent inverted flight as in an aerobatic aircraft. To implement this project, you need to have knowledge of CFD and Acusolve.
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