(Image removed from quote.)Kourage!
arlo, this is the wrong thread. Pictures of ayers go in saidforum btw you need a haircut
Absolutely not. WEP in AH recharges ad infinitum. Once the "cool down time" is over, you have full WEP again. You can do this cycle without end as long as you have fuel. That gives planes like the Ta 152H with it's 10/5 min cycle really an edge over those with a slower cycle.
The question I have is why the Merlins in American aircraft have a 5/5 minute WEP cycle and the Merlins in British aircraft have a 5/10 minute WEP cycle. This really puts WEP based fighters like the Mosquito Mk VI and Spitfire Mk XIV (Griffon, I know) at a relative disadvantage.
With little over 30 minutes flying time ( without etc-droptank) you will never get back a out-wepped 190 to normal temperature without reduce throttle very aggressively
I have the impression that the various cooling times are pretty arbitrary considering the very simple and generic way WEP is simulated.
There's a misconception in it: Reducing the throttle has no influence on "cool down" times. It's not based on temperatures, it's a function only depending on a timer.
I'd imagine so. I just want to know why my Merlins take 50% longer to cool off compared to a P-51's Merline. Heck, the Spitfire Mk IX and the P-51B have the same engine, just the Spitfire's is a Rolls Royce built Merlin 61 and the P-51B's is a Packard built Merlin 61 under an American designation. And it can't be the Packard vs Rolls Royce issue as the Spitfire Mk XVI and Lancaster Mk III (not that I have tested the WEP cycle on the Lancaster) both use Packard built Merlins.