Step 1: Reaction definition (compressor).
Stage reaction \(R\) is the fraction of the stage static enthalpy rise that occurs in the rotor:
\[
R \;\equiv\; \frac{\Delta h_{\text{static, rotor}}}{\Delta h_{\text{static, stage}}}
\text{with}
\Delta h_{\text{static, stage}}=
\Delta h_{\text{static, rotor}}+\Delta h_{\text{static, stator}} .
\]
A \(50%\)-reaction stage has \(R=\tfrac{1}{2}\).
Step 2: Consequence of \(R=0.5\).
\[
\Delta h_{\text{static, rotor}}
= \Delta h_{\text{static, stator}}
= \tfrac{1}{2}\,\Delta h_{\text{static, stage}} .
\]
Thus the rotor and stator each contribute half of the static enthalpy (and pressure) rise of the stage.
Step 3: Why options (A), (C), (D) are wrong.
(A) In an ideal compressor, the stagnation enthalpy increase occurs only in the rotor (work input), so \(\Delta h_{0,\text{rotor}}=\Delta h_{0,\text{stage}}\) (i.e., \(100%\), not \(50%\)). The stator ideally changes static pressure without changing stagnation enthalpy.
[2mm]
(C) \(R=0.5\) stems from symmetric velocity triangles; a common design is nearly constant axial velocity (\(V_x\) in = \(V_x\) out), not "half". Reaction says nothing about halving \(V_x\).
[2mm]
(D) With \(R=0.5\), \(\Delta p_{\text{static, rotor}}=\Delta p_{\text{static, stator}}\). Saying the rotor's rise is half of the stator's is incorrect wording; they are equal halves of the stage rise.
(Helpful triangle view)
For symmetric blading with constant \(V_x\): the whirl components satisfy \(V_{\theta 2}-V_{\theta 1} = \text{const}\) for the stage (Euler). The rotor raises static enthalpy by diffusion of relative flow; the stator raises static enthalpy by diffusion of absolute flow. Symmetry \(\Rightarrow\) each diffuses half the stage static rise \(\Rightarrow R=0.5\).
Final Answer:
\[
\boxed{\Delta h_{\text{static, rotor}}=\tfrac{1}{2}\,\Delta h_{\text{static, stage}}}
\]
A single-stage axial compressor, with a 50 % degree of reaction, runs at a mean blade speed of 250 m/s. The overall pressure ratio developed is 1.3. Inlet pressure and temperature are 1 bar and 300 K, respectively. Axial velocity is 200 m/s. Specific heat at constant pressure, \( C_p = 1005 \, {J/kg/K} \) and specific heat ratio, \( \gamma = 1.4 \). The rotor blade angle at the outlet is __________ degrees (rounded off to two decimal places).
In a centrifugal compressor, the eye tip diameter is 10 cm. For a shaft rotational speed of 490 rotations per second, the tangential speed at the inducer tip is _________ m/s (rounded off to one decimal place).