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#141
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I agree, the problems is how to model this in the sim. Crumpp replied earlier, and I have no objections at all, because that sounds very reasonable, the max speed stated was reached on an Aa engine, 2500RPM 1.45ata, rads 1/4 open (or closed). That plus some variation modelled, e.g. some Emils would do slightly more and some slightly less - that would be great.
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#142
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Interesting info about the Erla Gs, seen that one before on your website. Does not say anything about top speed being tested on the deck and I can't read the doc good enough to see the actual ata settings etc. |
#143
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I pointed out that typo already and it has been already corrected in the chart I am putting together, bugmenot.
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#144
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I don't know who put the variable s/c case frwd but the chart above posted by Bugmenot show precisely that there was none
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#145
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![]() Last edited by Robo.; 10-29-2011 at 03:42 PM. |
#146
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And again you're trying to make it sound as if every single test ever conducted on the 109E shows it not meeting proper speeds. Guess what? We don't have the data from every test ever. Stop trying to re-frame the issue based on your agenda. ---- I'm done engaging with you on this subject. You next post is going to be another one saying that the contractual obligations were actually just imaginary, theoretical numbers and blah blah. I don't have the patience to repeat the same facts over and over and have somebody just ignore it and say "but I think it's this way" so I will leave you to it. Last edited by CaptainDoggles; 10-29-2011 at 03:49 PM. |
#147
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I dunno how you conclude from bugemots chart that there had been no variation in speed from one plane to another. Actually Kurfürst's chart clearly provides proof that there had been significant scattering in speed. Indeed this chart is highly interesting as one might be able to transpose the scattering in speed to that one for the Emils. However it also prooves that the manufacturer's spec were likely spot on. So I now tend to think that there were 109E could indeed reach 500 kph or more. However it also shows that the real obtained mean value would probably be below the 500 kph because only three of the 13 managed to surpase the theoretical mean value of the spec. |
#148
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The mean certainly could have been lower than 500, but it just as easily could have been higher. This is why I think it's silly to use anything other than this figure. |
#149
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At least Microsoft was satisfied with testing only 13 aircraft. So why should we be less.
Oh, and I am very familiar with statistics. But I tend to adopt a pragmatic approach to problems. We do not have more than these 13 figures and we have to work with what we got. Anything else is just pure guessing around. |
#150
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![]() I am asking a simple question(s): Did they try to fly the airplane at full power at the deck as a part of the test? Did they verify the performance by attempting to achieve the top speed at any other altitude? They obviously did - and seeing the aircraft producing MFP / RPM expected, they simply assumed the curve as such was met within limits. We don't know, unfortunately, what ata they have been using. Other inspections (instruments, equipment etc.) were more important and if they were happy, they did not send the a/c back to get any issue fixed. How do you think the Emils in CoD should be modelled? Quote:
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