Tomorrow makes 2 weeks of RV-8A flying for me. I did receive transition training on all maneuvers including loops and rolls. Additionally, I have found the historical RVator articles on aerobatics quite helpful. Most notably Van's "An Aerobatic Epistle" (1998).
I have found aileron rolls quite fine at Va (123kts). I have been starting loops at 150-160kts, although, I will try some slower entry speeds to get the feel for them. I have experienced some of the "possible problems" pointed out by Van (most notably the "too much back pressure nearing the top of the loop" which inevitably leads to an accelerated stall at or just past the vertex of the maneuver--no big problem, just something to fine tune).
I was trying some "break turns" yesterday, just to get the feel for higher g-loading on the airplane, and found that, starting at Va, I was unable to apply more than 3.5 g's in a 90-100 degree banked turn without experiencing the buffet of an accelerated stall. I'm not sure if the airplane may be having a higher instantaneous g onset (that the Dynon accelerometer is not picking up), which is causing the stall, or if it is just the nature of the airplane. I'm thinking about putting a simple g meter in to test that theory, unless someone else has more insight.
What are others' experiences with g-loading on the airplane?
Troy