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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 Vmd |
B. | 1.216 Vmd |
C. | 1.3 Vmd |
D. | 1.2 Vmd |
Answer» B. 1.216 Vmd | |
4. |
What is Brequet Range expression? |
A. | R1 = \(\frac{D}{C}\frac{L}{V}\) ln ω |
B. | R1 = \(\frac{1}{C} \left[\frac{2W}{\rho S}\right]^{\frac{1}{2}} \frac{C_L^{\frac{1}{2}}}{C_D}\) ln ω |
C. | R1 = \(\frac{1}{V} \left[\frac{2W}{\rho S}\right]^{\frac{1}{2}} \frac{C_L^{\frac{1}{2}}}{C_D}\) ln ω |
D. | R1 = \(\frac{V}{C}\frac{L}{D}\) ln ω |
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. | |