Wind tunnel experiment on naca4415
Here on this experiment, it is befallen on students to study and experiment upon the pressure force distribution normal to the naca4415 airfoil, starting from α cl=0 till α= 18, and plot all the related graphs.
1. Introduction
- Objectives
- The naca 4415 airfoil
2. Observation
3. Theories and tables of data obtained
4. Observation
5. Angle of attack = 12 degree
6. Sample calculation
7. Error and recommendations
8. Conclusion
9. Reference