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This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Steam And Gas Turbines knowledge and support exam preparation. Choose a topic below to get started.
1. |
Aerodynamic center lies exactly at ______ on the chord from leading edge in cambered air foil. |
A. | half |
B. | one quarter |
C. | three fourth |
D. | none of the mentioned |
Answer» C. three fourth | |
2. |
Center of pressure lies exactly in ________ of the chord from the leading edge in a symmetrical air foil. |
A. | one quarter |
B. | half |
C. | three fourth |
D. | none of the mentioned |
Answer» B. half | |
3. |
Slope between lift coefficient and angle of attack in a line is __________ |
A. | 90 degree |
B. | 180 degree |
C. | 360 degree |
D. | 60 degree |
Answer» D. 60 degree | |
4. |
Relation between angle of attack and _______ for invincible fluids is found in thin airfoil theory. |
A. | Lift |
B. | Drag |
C. | Lift & Drag |
D. | None of the mentioned |
Answer» B. Drag | |
5. |
_________ difference is observed in between the sides of air foil. |
A. | Temperature |
B. | Pressure |
C. | Temperature & pressure |
D. | None of the mentioned |
Answer» C. Temperature & pressure | |
6. |
Cambered air foils generate lift at ________ angle of attack. |
A. | zero |
B. | high |
C. | low |
D. | none of the mentioned |
Answer» B. high | |
7. |
In air foil lift is __________ proportional to angle of attack. |
A. | inversly |
B. | not related |
C. | directly |
D. | none of the mentioned |
Answer» D. none of the mentioned | |
8. |
Air foils when designed to work in water are called as _________ |
A. | Dynamic air foil |
B. | Hydro foil |
C. | Dynamic air foil & Hydro foil |
D. | None of the mentioned |
Answer» C. Dynamic air foil & Hydro foil | |
9. |
In subsonic flight air foil has a shape of round at the leading edge. |
A. | True |
B. | False |
Answer» B. False | |
10. |
Airfoil when passed through fluids produces ______________ |
A. | thrust |
B. | drag |
C. | thrust & drag |
D. | none of the mentioned |
Answer» B. drag | |