If the static temperature rise in the rotor and stator respectively are \[\Delta {{T}_{A}}\] and \[\Delta T,B\] then degree of reaction in an axial flow compressor is given by:

\[\frac{\Delta {{T}_{B}}}{\Delta {{T}_{a}}+\Delta {{T}_{B}}}\]

\[\frac{\Delta {{T}_{A}}}{\Delta {{T}_{B}}}\]

\[\frac{\Delta {{T}_{A}}}{\Delta {{T}_{A}}+\Delta {{T}_{B}}}\]

\[\frac{\Delta {{T}_{B}}}{\Delta {{T}_{A}}}\]

If the static temperature rise in the rotor and stator respectively ar

1.	If the static temperature rise in the rotor and stator respectively are \[\Delta {{T}_{A}}\] and \[\Delta T,B\] then degree of reaction in an axial flow compressor is given by:
A.	\[\frac{\Delta {{T}_{A}}}{\Delta {{T}_{B}}}\]
B.	\[\frac{\Delta {{T}_{A}}}{\Delta {{T}_{A}}+\Delta {{T}_{B}}}\]
C.	\[\frac{\Delta {{T}_{B}}}{\Delta {{T}_{a}}+\Delta {{T}_{B}}}\]
D.	\[\frac{\Delta {{T}_{B}}}{\Delta {{T}_{A}}}\]
Answer» C. \[\frac{\Delta {{T}_{B}}}{\Delta {{T}_{a}}+\Delta {{T}_{B}}}\]

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If the static temperature rise in the rotor and stator respectively are \[\Delta {{T}_{A}}\] and \[\Delta T,B\] then degree of reaction in an axial flow compressor is given by:

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