Thanks IvanK,

Your climb tests tell a similar story to my speed at alt data.

The reference to +12psi and an external bleed hole confirms that the boost cutout used by Pilot Wilkie is the type modified for 100 octane emergency power. Blocking the drilled bleed hole returns the boost cutout to it's original operation (giving direct throttle control to the pilot) and hence the ability to get higher boost pressure than +12psi (on 100 octane).

camber

IvanK - thank you very much indeed! We've been doing some testing withe the RAF fighters against the 109s and we've also found serious discrepancies regarding performance.

Your time is much appreciated!

Not if you read the 1937 Flying Notes. It talks about this same modification independent of fuel. The boost override could allow the pilot to reach boost pressure which caused detonation and this a typical modification.

There is no way of telling from an anecdote the details of the engine modifications.

Using a bleed hole is a very common method to control boost pressures. This is the same thing that BMW took when increasing the BMW801D series to 1.58ata/1.65ata. They just drilled the hole on the other side of the diaphragm.

I am wondering what your expectations are here. Yes, the relative performance is about right. What is the issue???

The error looks to be on the order of about 10% which is not bad for climb performance.

You are asking the developers to correct performance to a standard day, too. They should be moving the opposite direction and modeling performance on a summer day.

Of course your climb rates are going to be significantly reduced at a high density altitude.

I would ask questions like:

"Why is my level speed matching performance corrected to standard on a high density altitude day?"

"Why is my radiator temperature hitting the upper limits in level flight on maximum continuous?"

"Why can I asymmetrically overload the airframe at 400 mph and nothing happens?"

There is a lot bigger fish to fry for the programmers than a small error in specific climb rates.

So Crumpp what then was the point of your comment in post #28 "Ok as close as possible is not exact." ?

I do actually agree with you in your comment on the Structural strength model (or lack of) in CLOD,and the other questions you propose as well. Other than standard Atmosphere question they have all been brought up directly with the devs a long time ago. When or if the devs decide to do something about them is for them to decide.

No it is not! Please have another look at the Spec graphs of E-4 and Mk.IIa and then have a look at the tests. You see? :grin:

Agreed on all this. I hope all this issues will be adressed at some point.

The error is not small! The gap is now ridiculous and very much unhistorical. Perhaps it does not matter to you for you don't actually fly this sim.

Absolutely disagree but this discussion occurred before and my position is essentially the same as Banks. No point to reopen the argument here.

http://forum.1cpublishing.eu/showthr...t=32190&page=2

+1
i enjoy to fly with my squad mates, and against our other squads on the RAF side....im a 109 guy, and fighting against RAF with the current flight models isnt fun at all.
its way too easy now for the 109s.it would be boring, if this performance difference between LW and RAF planes was correct, but its not and therefore its annoying as well.
i want them all as accurate as possible.

thx IvanK for using your time to test, and furthermore to help the devs with documents.though its a bit puzzling, that the devs really "need" your information at all.

When error due to the scale is considered the SPITII and 109 climbing times are considered equal when compared each other in both (RL and GAME). There is an error in measuring due the scale (due the human eye that placed the points there), an error due the measuring (since the human pilot is not perfect). If you create an error bar considering all sources of error the bars would superpose themselves, then you can consider both very well matched. Sorry for my bad english but i expect that you understand. Statistically both are well matched. You see a gap between both, but this can be only because the error margins, due the imprecision of the human eye and from the instruments of measuring.:cool:

Ivank

Can you provide your measurements in table format? I will plot the data in ORIGIN and calculate the error bars.

ORIGIN: http://www.originlab.com/

Ernst if you try to follow a 109 in the climb, you'll see the gap is very much real :D

I appreciate you're trying to get the measurment methodic right, but the fact is the RAF aircraft are, unfortunately, seriously underperforming - no matter how you're looking at it.

Or even better, I suggest you do your own tests and share them with us.

Regards.

Conditions very much matter in aircraft performance and if they do not match, do not expect the same performance.