MCQOPTIONS
Saved Bookmarks
This section includes 8 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Performance knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
Which of the following does range factor consists? |
| A. | Air density |
| B. | Cruise weight |
| C. | Temperature |
| D. | Cruise weight and air density |
| Answer» E. | |
| 2. |
What is range factor in cruise method 1? |
| A. | ( left[ frac{V_{mdi}}{C} E_{max} right] ) |
| B. | ( left[ frac{V_{max}}{C} E_{max} right] ) |
| C. | ( Big { frac{2u^3}{u^4+1} Big } ) |
| D. | ( Big { frac{2u^4}{u^4+1} Big } ) |
| Answer» B. ( left[ frac{V_{max}}{C} E_{max} right] ) | |
| 3. |
Brequet Range expression value is maximum at __________ |
| A. | 1.316 V<sub>md</sub> |
| B. | 1.216 V<sub>md</sub> |
| C. | 1.3 V<sub>md</sub> |
| D. | 1.2 V<sub>md</sub> |
| Answer» B. 1.216 V<sub>md</sub> | |
| 4. |
What is Brequet Range expression? |
| A. | R<sub>1</sub> = ( frac{D}{C} frac{L}{V} ) l<sub>n</sub> |
| B. | R<sub>1</sub> = ( frac{1}{C} left[ frac{2W}{ rho S} right]^{ frac{1}{2}} frac{C_L^{ frac{1}{2}}}{C_D} ) l<sub>n</sub> |
| C. | R<sub>1</sub> = ( frac{1}{V} left[ frac{2W}{ rho S} right]^{ frac{1}{2}} frac{C_L^{ frac{1}{2}}}{C_D} ) l<sub>n</sub> |
| D. | R<sub>1</sub> = ( frac{V}{C} frac{L}{D} ) l<sub>n</sub> |
| Answer» E. | |
| 5. |
Which of the following is incorrect statement regarding cruise method 1? |
| A. | W/D ratio is kept constant |
| B. | L/D ratio is varying |
| C. | Air pressure is decreased |
| D. | Aircraft weight is decreased |
| Answer» E. | |
| 6. |
Cruise climb technique is involved in ___________ |
| A. | cruise method 1 |
| B. | cruise method 2 |
| C. | cruise method 3 |
| D. | cruise method 4 |
| Answer» B. cruise method 2 | |
| 7. |
What is the condition of cruise method 1? |
| A. | Air pressure is increased |
| B. | Aircraft weight is increased |
| C. | W/D ratio is kept constant |
| D. | L/D ratio is varying |
| Answer» D. L/D ratio is varying | |
| 8. |
In cruise method 1 the air pressure is decreased whereas the aircraft weight is increased. |
| A. | True |
| B. | False |
| Answer» C. | |