The airspeed indicator does subtraction in the process of indicating speed. Airspeed is the difference between the static port pressure and the pitot tube pressure.
A static source on the left side of an aircraft will indicate correctly only when the relative wind provides no ram or vacuum effect on the static port. In a slip, high or low airspeed variations will occur depending on the direction of a slip. In a slip the airspeed error cannot be predicted.
Slipping into the static port causes ram air effect on the port. Thus the difference between the static air pressure and the pitot air pressure will be less. Indicated airspeed will be less. Any time the relative wind is not directly into the pitot tube the pressure will be lower. The result is a lower indicated airspeed unless countered by the much greater effect of static port pressure. Relative wind is any wind created by motion will act opposite to the direction of motion.
Now a stall occurs when the wing exceeds the critical angle of attack and the airflow delaminates from the wing surface. Is this a danger during a slip? Of course. But how should we regard the relative wind since it is striking the leading edge at an angle, effectively making a longer wing chord? Should the IAS be trusted as our actual airspeed, or disregarded as erroneous?
The forward slip is an important technique for getting into some backcountry strips, so you guys must have given this some thought.
Zane

