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| 1. |
What is the reason for a sudden increase in drag beyond drag divergence? |
| A. | Transonic region on top surface of the airfoil |
| B. | Supersonic region on top and bottom region of the airfoil |
| C. | Prandt- Glauert compressibility effect |
| D. | The shape of the airfoil |
| Answer» C. Prandt- Glauert compressibility effect | |