Tools
Performance Tool
Validation Tool
Aim
Theory
Pretest
Procedure
Simulation
Posttest
References
Contributors
Feedback
Aim
Theory
Pretest
Procedure
Simulation
Posttest
References
Contributors
Feedback
Surface pressure distribution over airfoil NACA 0015
Objective:
To measure the Coefficient of pressure distribution and
To find the Coefficient of lift of the airfoil NACA 0015.