Concept:
Armature reaction refers to the effect of the armature mmf (magnetic motormotive force) on the main field flux distribution of a synchronous machine. The nature of this armature reaction depends entirely on the power factor ($\cos\phi$) of the connected load, which determines the spatial phase angle between the internal induced EMF ($E_f$) and the stator armature current ($I_a$).
Step 1: Analyze the circuit parameters under short-circuit conditions.
During a steady-state short-circuit fault at the terminals of a synchronous generator, the external load impedance drops to zero. The circuit is limited only by the internal machine impedance:
\[
Z_s = R_a + jX_s
\]
In standard large synchronous machines, the armature resistance $R_a$ is negligible compared to the synchronous reactance $X_s$ ($R_a \ll X_s$). Therefore, the short-circuit impedance is almost purely inductive:
\[
Z_s \approx jX_s = X_s \angle 90^\circ
\]
Step 2: Determine the phase relationship between voltage and current.
The short-circuit armature current $I_{sc}$ is given by:
\[
I_{sc} = \frac{E_f}{Z_s} \approx \frac{E_f \angle 0^\circ}{X_s \angle 90^\circ} = \frac{E_f}{X_s} \angle -90^\circ
\]
This shows that under short-circuit conditions, the armature current $I_a$ lags the internal generated voltage $E_f$ by exactly $90^\circ$. This condition corresponds to a purely lagging zero power factor (ZPF lagging).
Step 3: Evaluate the spatial orientation of the magnetic fluxes.
* The main field flux ($\phi_f$) produces the maximum induced voltage $E_f$ when it is shifted $90^\circ$ ahead of it in space.
* Since the current lags $E_f$ by $90^\circ$, the armature reaction flux ($\phi_a$) aligns directly opposite to the main field flux ($\phi_f$).
\[
\phi_{\text{resultant}} = \phi_f - \phi_a
\]
Because the armature magnetic field acts directly against the main rotor field flux, it reduces the net flux, which is a purely demagnetizing effect.
Consequently, the armature reaction is purely demagnetizing, which matches Option (B).