In the context of a multistage axial flow compressor, understanding how axial velocity behaves across different stages is crucial. Each stage of the compressor is designed to compress the air further, but certain parameters are maintained to ensure efficiency and stability. The axial velocity is one such parameter. Here's why it remains the same:
The axial velocity is kept constant across various stages due to the principle of optimal design of compressors. This consistency is essential for several reasons:
Therefore, in a well-designed multistage axial flow compressor, the axial velocity typically remains the same across the higher stages to ensure optimal performance and reliability.
At the design conditions of a single-stage axial compressor, the blade angle at rotor exit is \(30^\circ\). The absolute velocities at rotor inlet and exit are 140 m/s and 240 m/s, respectively. The relative flow velocities at rotor inlet and exit are 240 m/s and 140 m/s, respectively. Find the blade speed \(U\) at the mean radius (round off to two decimal places). 