I’ll try to explain more the phenomenon:
The actual schematic diagram of an induction motor it is similar with a transformer.
The difference is the rotor side impedance and output voltage depends on s[slip].Slip is related to the difference between the magnetic field rotation-equal to the synchronous speed-a bit more than no-load speed- and the actual rotor speed. It changes all the time- from start =1 to 0.02-0.05 at full load:
s=(synchronous speed-actual speed)/synchronous speed.
The reactance is changing more since depends also directly on slip since the rotor current frequency f=frated*s
That means for 60 Hz at s=1 [start] f=60 and for full load it could be 0.05*60=3 Hz
If the rotor side of the diagram will be divided by nst/nr[stator number of turns/rotor number of turns] and by s then we may attach this to the stator side:
Let's say the rotor is a squirrel cage short-circuit rotor then V'r=0
At start the Io[the magnetic core equivalent current] is negligible we have this:
Vst=Ist*[(Rst+R'r/s)+j(Xst+X'r)]
For start this formula is close to the actual. For other slip this it is only informative.
What we know then we have an impedance at start [this is the minimum] and other impedance at other s [and maximum at the no-load steady].
Let’s take an induction motor of 200 kW at 440 V A Ilockrot=6*Irated
Irated=381 A[line current] but the current in the transformer windings connected in delta will be 381/sqrt(3)=220.1 A. and cos(φ)=0.86 Z=440/220=2
So let's say 1.72+j1.02 [Z=sqrt(1.72^2+1.02^2)=2] it is the impedance at full load [when R/s could be significant]
At start D.O.L-across the line- [in delta line current ] IstD=Ilockrot=6*Irated=2288.7 A and p.f.[cos(φ)]=0.3 then Zst= 0.1+ j0.32 at start [Z=0.333].
At start, connected in star, the voltage will be only 440/sqrt(3)=254 V per phase and the current at start will be 0.33*IstD=762.9 A[254/.333=763.7A]