Razgriz10

Can confirm it is not working at the moment.

20 degrees is what was in the mission editor settings so yeah you're probably right about that. I'll check again tomorrow and get the actual temperatures.

My Testing at 22400ft, 29.92inHg, 20 degrees Celsius, 50% internal fuel, 54.9inHg manifold pressure and 2700rpm yielded a maximum level flight speed of 240kts indicated. Calibrating that using the manual is 246kts, then plugging that into an online calculator for TAS i got 385kts. then converting to mph i got 443mph which is 18mph faster than the real plane and is in fact closer in speed to the -4 variant with a maximum level flight speed of 446mph. Attached are screenshots from my run (ignore the slight rate of climb, i bumped the stick while pausing and it was less than half a second of climb) and of the manual and calculator used (the conversion from Knots to mph i did on my phone).

I'll test it when i can but i suspect flight in a massive skid would also cause the speed reduction that people are talking about, but from my flying it seems pretty spot on the charts that i have seen.

RPM should not be affected at all by introduction of water injection, you will only get a change in manifold pressure. In the Corsair that is an increase from about 53in Hg in military power, to about 59in Hg in WEP. Both of those power settings are at 2700 rpm. If you are in level flight, proberly trimmed, and have all the cooling shutters as closed as they can be to maintain temps with in allowable limits you can get about 300 knots indicated at around 10000ft in military power, which is almost bang on where it is supposed to be. What i suspect a lot of people are doing is opening the oil cooler shutters or the cowl flaps to much, both of which cause a lot of drag.

Please, the current sounds are quite lackluster. Even if you don't want to pair with E19 for some reason, please work on the sounds.

Are you in trim? Because if you are in a skid then you wiil be very slow.

Bro, this is a big leagal issue going on between two companies. They are not going to publicize things about internal disputes until things are resolved however that may end up and even then we may never know everything. We are all just going to have to deal with that fact. They have left the optioin open for refunds and told us everything that they can at the moment. If you don't like it then tough luck.

I highly disagree with your assesment of the F-5. It may not be very complex but thats just how the airplane is and is a great moduel.

The reason the plane is shaking above 1.45 ata is because you are causing engine knock above 1.45 ata. The MW50 is used to prevent knock and allow higher manifold pressure and therefore more power. The limit of 1.45 is mostly due to the fuel octane rating, B4 has roughly 90 octane while german C3 has about 100 octane. Other versions of the DB605 uses C3 without MW50 and can run the same manifold pressure as the other version with it. This is why the D9 also has MW50 normaly used where as the P-47 has a smaller amount and can produce much more manifold pressure because it uses a higher octane fuel, i belive 130 octane is the dcs version.

Razgriz F86