Aerospace Engineering > GATE 2014 > Axial Compressors
For a fifty percent reaction axial compressor stage, following statements are given:
I. Velocity triangles at the entry and exit of the rotor are symmetrical
II. The whirl or swirl component of absolute velocity at the entry of rotor and entry of stator are same. Which of the following options are correct?
I. Velocity triangles at the entry and exit of the rotor are symmetrical
II. The whirl or swirl component of absolute velocity at the entry of rotor and entry of stator are same. Which of the following options are correct?
Correct : b
Similar Questions
In a 50% reaction axial compressor stage, the local blade velocity is 300 m/s and the axial component of velocity is 100 m/s If the absolute inlet flow angle &a...
In a 50% reaction axial compressor stage, the local blade velocity is 300 m/s and the axial component of velocity is 100 m/s If the absolute inlet flow angle &a...
In a 50% reaction axial compressor stage, the local blade velocity is 300 m/s and the axial component of velocity is 100 m/s If the absolute inlet flow angle &a...
Total Unique Visitors
Loading......