What would exactly happen when flaps are either a) deployed at high speed, or b) already deployed when the plane reaches high speed?
I'm curious of what would happen, because I did a simple test during discussions about flaps in 1C:Maddox's IL-2 forums.
Now, I've heard the flap modelling had some problems in IL-2, but I was surprised to find out how seemingly, undeniably porked they were when the test results were as following:
1) When the flaps are deployed before high speeds are reached, the flaps jam at approximately 750kph(460mph)
2) When flaps are deployed after high speeds are reached, the flaps jam at approximately 750kph(460mph)
3) With maximum throttle and WEP engaged, in a 45 degrees dive with full flaps engaged, at speeds of approximately 680kph(418mph), the lift force generated by the flaps actually pushes the plane upwards up to a degree which the pilot cannot fight it even when pushing the stick forward in full deflection.
The flaps are so strong that they endure the 680kph(418mph) dive, ignores the pilot input of stick forward full deflection, and pushes the nose pitch upwards and reduces speed.
4) With full flaps engaged, only a near-vertical dive reaches speeds over 700kph(430mph) and makes it possible to get the flaps jammed.
......
So I'm curious.. let's say a certain plane has flap deployment maximum speed limit at 200mph.
1) If a plane deploys its flaps at 210mph, will it immediately jam? Or is the 200mph line something like the "expiration date" on milk cartons? A maximum "safety" line, no guarantee what would happen if flaps are deployed over that 200mph line?
2) If the same plane attempts to deploy its flaps at 400mph, will it instantly jam or tear off?
3) If the plane already has flaps deployed at 180mph, and then crosses over 200mph line, will the results be somewhat different than when the flaps were deployed after the limit was reached?
4) Can any WW2 plane in a full flap configuration endure a 418mph dive without the flaps breaking off?
5) If we just assume there's a flap that can endure high speeds, is it possible that during a 45 degrees dive at high speeds the lift force generated by the flaps just pushes the plane's pitch upwards, denying the full forward deflection input?
6) The test I have done, in order to reach high speeds quickly, started off from 10000 meters, making it easy for the plane to just dive and catch speed. Would there be differences in how the flaps can endure pressure at high alts and low alts?