Worked under the guidance of Dr. C.S. Upadhyay, and developed a computational aeroelastic model to analyze different wind conditions acting on an aircraft wing at different materials, angles of attack, thickness, and Reynolds number. Then I tested the model at different Mach numbers to obtain the pressure distribution profile and the oscillation-prone areas. Finally, I Optimized the results to get a desired maximum bending limit of the wing for different materials.