italian harvard wrote:
My personal opinion, based on my modest experience of aerobatic flying, is that he wanted to go for a loop or half cuban 8, but the climb was too steep and he didnt cut the throttle while reaching the top, this causing a rotation induced by the prop and engine torque (hence the innatural but smooth rotation). Once inverted on top he let the plane go (applying opposite controls would have been fatal), until he gained speed again and did some rudder overcontrol to counteract the roation (he prolly prepared himself to counteract a spin). My only remark is about height: we know of the peculiar display area of la fertè alais, but anyway I'd focus my efforts on requiring more severe parameters about height and aerobatic programs.
My 2 €urocents, hope u dont mind

Cheers
Alex
What??? What are you people talking about??? I can't understand any of that? Let's look at this again...
"...he wanted to go for a loop or half cuban 8, but the climb was too steep and he didnt cut the throttle while reaching the top"
I don't know what is meant by "the climb was too steep", but if you're going to execute a loop or any other over the top maneuver you're going to have to fly past vertical. When performing over the top maneuvers you don't reduce power until established on the down line, unless you want to perform a tail slide.
"...this causing a rotation induced by the prop and engine torque (hence the innatural but smooth rotation). Once inverted on top he let the plane go (applying opposite controls would have been fatal), until he gained speed again and did some rudder overcontrol to counteract the roation (he prolly prepared himself to counteract a spin)."
I've read this seven times and I have no idea what it means. "Applying opposite controls would have been fatal". Huh? After the aircraft runs out of energy and reaches what is basically a zero airspeed state the Bf-109 begins to enter a spin. At this point the aircraft has departed controlled flight and the pilot is now a passenger. It appears he does unload the elevator and is also probably applying opposite rudder, at which point the aircraft recovers and the pilot regains control, departing the area at approx a 90 degree divergent heading.
This is NOT about height, it's about energy. The Bf-109 pilot did not have enough kinetic energy (airspeed) to successfully complete the maneuver. If he had, say another 50 or 75 knots of airspeed then the loop would have been completed with a more than sufficient altitude cushion. However, once the aircraft stalled and began to spin it was necessary to convert the potential energy of altitude into kinetic energy of airspeed in order to regain control of the aircraft.
We don't need to perform aerobatics at greater altitude, we need to not stall/spin while performing display aerobatics. Very embarassing, especially when captured on video.
I went out yesterday and flew the Sea Fury to set a minimum energy state for "over the top" maneuvers. This is something I learned from aerobatic flying in the L-39, but I needed to work out the numbers for the big Hawker, as I hadn't done it yet. After that (with this debate in mind) I decided to enter a loop at an airspeed I knew didn't give me enough energy to complete the maneuver (160 knots).
Anyone want to guess what happened?