MCQOPTIONS
Saved Bookmarks
MCQOPTIONS
This section includes 3 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design Questions and Answers knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
If an airfoil has lift of 200 N at 10° AOA, then what is induced drag produced by airfoil at that AOA? |
| A. | 0 N |
| B. | 100 |
| C. | 0 |
| D. | 100 N |
| Answer» B. 100 | |
| 2. |
An aerofoil is operating with flow velocity of 100m/s. Aerofoil is symmetric and is at 0° AOA. Determine lift produced by this aerofoil. |
| A. | 10.5 N |
| B. | 0 N |
| C. | 50 N |
| D. | 100N |
| Answer» C. 50 N | |
| 3. |
The parameter marked by ’?’ in the diagram is _____ |
| A. | trailing edge |
| B. | leading edge |
| C. | chord |
| D. | camber |
| Answer» B. leading edge | |