HWD
Think outside of the box...
In a standard stall, when the critical alpha is reached or exceeded, the relative airflow around the aerofoil is disturbed and lift is reduced.
An accelerated stall is not the same as a "Standard" stall. The problem is that the increased wing loading means that the aerofoil is not producing enough lift to oppose the effect of gravity or "g". This is why there is a relationship between IAS and G. The higher the g, the more airspeed you need to generate more lift to counteract the wing loading. Think of it as a "heavy" aircraft. You would need a faster Vr to get airborne at heavy weight than at light weight because the wing needs to produce more lift to overcome weight/gravity.
Hope that is a bit clearer...