For axial flow compressor, the reaction ratio in terms of rotor blade angle at inlet (β1), at outlet (β2) and flow coefficient (θ) is

1
2ϕ (tan β1 - tan β2)
2
2ϕ (tan β1 + tan β2)
3
\(\frac{\phi}{2}(tan\beta _1 ~-~tan\beta_2)\)
4
\(\frac{\phi}{2}(tan\beta _1 ~+~tan\beta_2)\)

Sponsored

hivanix.in

Visit

This quiz is brought to you by hivanix.in

🌐 Web App Development

Quick Navigation