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This section includes 8 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design knowledge and support exam preparation. Choose a topic below to get started.
1. |
We should always use tail dragger arrangement for every aircraft. |
A. | True |
B. | False |
Answer» C. | |
2. |
An aircraft is supported by bicycle landing gear arrangement. If wheel base is 10 unit then, scale location of CG. |
A. | 5 unit aft from front wheel |
B. | 10 unit |
C. | 20 unit from front wheel |
D. | 25 unit from back wheel |
Answer» B. 10 unit | |
3. |
What is tipback angle? |
A. | Maximum attitude of an aircraft with tail touching the ground with struts fully extended |
B. | Wing loading divided by span |
C. | Lift to drag ratio |
D. | Maximum altitude of an aircraft |
Answer» B. Wing loading divided by span | |
4. |
The term marked by ‘?’ in the following diagram is called __________ |
A. | Overturn angle |
B. | Overnose angle |
C. | Grazing angle |
D. | AOA |
Answer» B. Overnose angle | |
5. |
Which of the following is disadvantage of tail dragger? |
A. | Inherent unstable |
B. | Most stable |
C. | Inherent stable |
D. | It has 4 wheels to support the aircraft |
Answer» B. Most stable | |
6. |
What is the location of main wheel in tricycle gear? |
A. | After CG of the aircraft |
B. | At CG |
C. | Before CG |
D. | At nose |
Answer» B. At CG | |
7. |
What is the following is correct? |
A. | Quadricycle landing gear arrangement requires Flat takeoff attitude |
B. | Lift is always same as weight |
C. | Drag is always higher than weight |
D. | Thrust loading is weight to lift ratio |
Answer» B. Lift is always same as weight | |
8. |
Typically, an aircraft weighing lower than 50000 lb will adopt __________ |
A. | single main gear |
B. | bicycle |
C. | tail dragger |
D. | tricycle |
Answer» B. bicycle | |