1. Relative velocity at the inlet and exit of the rotor blades are the same. |
2. Absolute velocity at the inlet and exit of the rotor blades are the same. . |
3. Static pressure within the rotor blade channel is constant. |
4. Total pressure within the blade channel is constant. |
A) 1 and 4 are correct
B) 2 and 3 are correct
C) 1 and 3 are correct
D) 2 and 4 are correct
Correct Answer: A
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