Originally posted by moot
Widewing, please compare with the pre 2.06 (or AH1 to be sure) Ta152. You won't even have to do a whole battery of tests to see the differences.
They'll be most obvious in tight and twisty ACM.
edit- I just re-read your post and you're basicaly saying there is nothing unstable about the 152 anywhere in landing, lowspeed dogfight ACM, sustained flat turns, and airspawns.... WW, with all due respect, you're doing something wrong and/or very different with what just about everyone else who's flown the 152 has reported.
I'll post movies if needed...
Well, I don't think I'm doing anything wrong, inasmuch as I don't encounter the same problems.
I loaded AH1 and took off in the Ta 152 with 25% fuel. I then performed a turn radius test. Speed taken from film.
At 500 feet I sustained 124 mph for three consecutive circles, which took 63.16 seconds. Thus, 124/60= 2.067. 2.067x5820=10911.999. 10911.999/60=181.867. 181.667x63.16=11486.70. 11486.70/3=3828.90 3828.90/3.14=1219.39 (average turn diameter). 1219.39/2=609.7 (average turn radius).
I then loaded AH2 and took off in another 152 with 25% fuel. I performed the same test. Speed taken from film.
At 500 feet I sustained 127 mph for three consecutive circles, which took 62.06 seconds. Thus, 127/60=2.117. 2.117x5280=11176.00. 11176.00/60=186.27. 186.27x62.06=11559.71. 11559.71/3=3853.24. 3853.24/3.14=1227.14 (average turn diameter). 1227.14/2=613.57 (average turn radius).
So, the difference between the turn radii between AH1 and AH2 is less than 4 feet. Well within the average deviation expected (which I classify as +/- 3%). In short, they are virtually identical in this aspect of performance. One can reduce this 10 to 15 feet by pushing a bit harder, but the result is usually a substantial reduction is turn rate. This trade-off isn't usually desirable.
Another advantage of AH2 is the superior stall warning. There's no cockpit shake in AH1, so all you have for warning is the stall horn. AH2 gives plenty of advanced warning with the stall horn and increasing cockpit shake. In short, it's easier to avoid a stall in AH2. Especially for newer pilots.
Krusty is apparently shocked that I don't get flat spins on air spawns. That's probably because I use a better technique upon spawning. As soon as I spawn, the stick goes full forward and I raise the gear and start the engine (all in about 2 seconds). The plane rolls to the left and I center the stick and now counter torque with right rudder. Rotation stops with the nose down and I feed in power and level off... No sweat, no hassle, no spin, no tail slide, no drama. I'll post a film.
Now, it's certainly possible to induce a tail slide by over-flying the 152. Sudden and large elevator inputs while flying near pure vertical will induce these (and do so in many aircraft). However, it is very easy to recover from. Simply press E to shut off the motor. The nose pitches down instantly and you restart. There's very little loss of altitude. Again, I'll post a film.
I'm not having the troubles you gents are.. So, the question begs; what are you doing to induce this behavior? Post some films if you can, it may help to figure out where the problem is.
As to landing... The AH1 Ta 152 is less darty on the runway. The AH-2 152 tends to hunt from left to right. But, lots of AH2 fighters do that, such as the P-51D and F6F-5. The secret to avoiding this is to 3 point your landings. This is something I do in all tail-draggers. That's why I never suffer a ground loop. My point is, if you can land an F4U without undue drama, the Ta 152 is no sweat.
My regards,
Widewing