QUESTION $01-$ Axial Flow Compressor

The following is the data of the Axial Flow Compressor. Using this, find air angles, mass flow per sec$,$ Input power of the compressor, Stagnation temperature rises per stage, stagnation temperature ratio, and stage loading coefficient.

$\backslash$table$[[$Parameter$,$Units$],[$Inlet pressure and temperature,$1$ bar and $300$ K $,$ respectively$],[$Degree of Reaction,$50\%],[$Mean blade diameter,$36$ cm$],[$Rotational speed,$18000$ rpm$],[$Blade height,$6$ cm$],[$Air angle at rotor and stator,${25}^0$