Spit/109 sea level speed comparisons in 1.08 beta patch

[camber]

I had a sad 109 experience yesterday. Flying in overcast it is easy to get confused between the top and bottom of the aircraft, leading to the following:

Originally Posted by 5./JG27.Farber

Test 4 4500metres 1.3Ata 2400U/pm IAS 400 TAS 518 or 322 mph
Test 5 5000metres 1.23Ata 2400U/pm IAS 390 TAS 518 or 322 mph
Test 6 4900metres 1.15Ata 2200U/pm IAS 370 TAS 489 or 304 mph

http://youtu.be/O4jHSMyYdkg <---- Video of tests.

Now we need to dig out the real life tests and compare.engine in the usual way
.

Seeing as you are doing some altitude 109 tests I did the same on patch 1.08. It seems not to have changed the last two patches though.

At 5000m 1.23ata 2400rpm I get IAS 400kmh which seems consistent with your Test 5 above.

The 109 does not change max speed between 2100 and 2400rpm which simplifies things.

Messerschmitt "guaranteed" top speed: (backed up by the flight test record)

570kmh TAS @ 5000m, 2400rpm, 1.3 ata (5 min limit).

CloD 109E4 (manual prop pitch) top speeds:

425kmh IAS = 561kmh TAS @5000m, 2400rpm, 1.32 ata

Full throttle boost has dropped below 1.35ata at 5000m. However the 109 1 minute takeoff boost is still working and oddly enough will still increment boost at 5000m (to 1.42ata).

440kmh IAS = 581kmh TAS @5000m, 2400rpm, 1.42ata.

So the CloD 109E4 at 5000m is 10kmh slow at the 1.3ata combat setting (will assume boosts in the 1.3-1.35ata range can be considered effectively the same). However it has access to the takeoff boost at altitude, which enables it to be 10kmh faster than the real life version.

Cheers, camber

Offline tests, cockpit off, speeds rounded to 5kmh, 4950-5050m, oil/water rads fully open, OAT 25/1000ft rule for IAS/TAS conversion.