Yaw was present, I was fighting it the whole time, and then in the end, I reduce throttle, the cut it completely.
You can think of it like pre-loading the controls, and setting yourself up to let the plane, yaw and roll into a position that leads your advantage. The the mossy up and get some airspeed, say 250mph. Put the mossy into the vertical make it stall straight up, and then fall backwards back to the earth.
Once you can do that, gather airspeed again and climb vertical, now try to time your inputs so that you can achieve a similar stall to what the video shows. Too early on the inputs, your flight path become a large turn. Too late in the inputs, you tumble to the ground.
Try letting your airspeed get down to about 100mph, and then kick rudder until your nose it at about 10 or 11 o'clock. As soon as you reach this yaw angle, cut throttle, but hold your rudder and aileron where they are. With practice you can do it.
I was suprised to see that no YAW was induced until the airspeed was decreased to 16MPH. The engins were in WEP. I question the model. There is no way that YAW would not have been present due to PFactor and Gyroscopic progression.
As I tried to show in my diagrams, the rudder did not cause the yaw at 16mph, that yaw was induced by the factors mentioned in your statement.