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This section includes 15 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. |
What will be the pressure-height ratio of air at an altitude of 9144m? (L0=-0.0065 K/m, T0=288.15K, P0=101325 N/m2) |
A. | 0.297 |
B. | 0.596 |
C. | 0.359 |
D. | 0.458 |
Answer» B. 0.596 | |
2. |
What is relative pressure at 1600ft? (P1600=95602 N/m2) |
A. | 0.9453 |
B. | 0.9858 |
C. | 0.9435 |
D. | 0.9595 |
Answer» D. 0.9595 | |
3. |
What is relative temperature at 1600ft? (T1600=284.98 K) |
A. | 0.989 |
B. | 0.838 |
C. | 0.877 |
D. | 0.999 |
Answer» B. 0.838 | |
4. |
What is relative temperature at 241.45K? |
A. | 1 |
B. | 0.8379 |
C. | 0.8774 |
D. | 0.8756 |
Answer» C. 0.8774 | |
5. |
What is relative pressure at 101325 N/m2? |
A. | 1 |
B. | 2 |
C. | 3 |
D. | 4 |
Answer» B. 2 | |
6. |
Any atmosphere that does not conform to the ISA profile is referred to as an off-standard atmosphere. |
A. | True |
B. | False |
Answer» B. False | |
7. |
The pressure-height relationship in troposphere is given by _______ |
A. | \(\frac{p}{p_0}\)=[1 + \(\frac{L_0}{T_0}\)H]\(\frac{-g_0}{RL_0}\) |
B. | \(\frac{p}{p_0}\)=[1 + \(\frac{L_0}{T_0}\)H]\(\frac{-T_0}{RL_0}\) |
C. | \(\frac{p}{p_0}\)=[1 + \(\frac{g_0}{T_0}\)H]\(\frac{-g_0}{RL_0}\) |
D. | \(\frac{p}{p_0}\)=[1 + \(\frac{L_0}{g_0}\)H]\(\frac{-g_0}{RL_0}\) |
Answer» B. \(\frac{p}{p_0}\)=[1 + \(\frac{L_0}{T_0}\)H]\(\frac{-T_0}{RL_0}\) | |
8. |
The difference between true height and geopotential height is relatively small. |
A. | True |
B. | False |
Answer» B. False | |
9. |
What is the pressure difference across a cylinder which consists of water and has a height difference of 20m? |
A. | -196.2 kN/m2 |
B. | -1.962×10-5 bar |
C. | -196.2 kN/m2 |
D. | -1.962×10-5 bar |
Answer» B. -1.962×10-5 bar | |
10. |
What is the hydrostatic equation? |
A. | ΔP=-ρg∆h |
B. | ΔP=-ρgh |
C. | P=-ρgΔh |
D. | ΔP=ρgΔh |
Answer» B. ΔP=-ρgh | |
11. |
What is true height? |
A. | The vertical geometrical distance between an object and a datum level |
B. | The vertical geometrical distance between a certain height and a datum level |
C. | The horizontal geometrical distance between an object and a datum level |
D. | The horizontal geometrical distance between a certain height and a datum level |
Answer» B. The vertical geometrical distance between a certain height and a datum level | |
12. |
What is lapse rate? |
A. | Change of temperature with respect to altitude |
B. | Change of temperature with respect to pressure |
C. | Change of pressure with respect to altitude |
D. | Change of temperature with respect to density |
Answer» B. Change of temperature with respect to pressure | |
13. |
The temperature-height profile is given by ___________ |
A. | T=Ti+Li (H-Hi) |
B. | T=Ti+Li (H+Hi) |
C. | T=Ti-Li (H-Hi) |
D. | T=Ti-Li (H+Hi) |
Answer» B. T=Ti+Li (H+Hi) | |
14. |
According to ISA atmospheric model what is the value of datum atmospheric air density kg/m3? |
A. | 1.225 |
B. | 12.225 |
C. | 1.23 |
D. | 1.000 |
Answer» B. 12.225 | |
15. |
International Standard Atmosphere is based on the assumption that air is a perfect gas and obeys gas law. |
A. | True |
B. | False |
Answer» B. False | |