Rich, thanks for answering my initial question.
Hi Diana, you're welcome!
Two more things to note if you do the exercise with partial power:
First, you may not need to pull the stick/yoke all the way aft -- just pull it far enough aft to encounter the onset of stall buffet, then hold that position until you decide to stop.
Second, the Citabria has sufficient rudder authority to correct much greater heading deviations than something like a Cessna 150 or 172.
In the 150/172, your "window of controllability" is about 20 degrees wide on either side of the original heading. Once the airplane deviates beyond that, even full opposite rudder applied and held will not return the airplane to the original heading. There is, however, sufficient rudder authority to prevent a spin. So the airplane ends up performing a stalling, slipping, spiral -- not able to return to heading, not spinning, just bobbing in and out of stall buffet as it spirals down in a slip. If one were so inclined, you could execute a 360 degree turn in this manner, without any increase in airspeed.
Since this would then be a slipping, turning stall, the recovery is straightforward: break the stall (stick/yoke forward), return to coordinated flight (release the rudder input), return to straight & level.
BTW, on the off chance that anyone here might be interested, I'm trying my hand at a new blog:
www.richstowell.com/blog
Rich
www.richstowell.com