Quote:
Originally Posted by Crumpp
Once again, an argument of your own determination. The specific performance determination for an individual aircraft has not ever been disputed with the exception of pointing out that you do not couple the affects and take the calculation to it's conclusion.
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I think that I have said several times that the polar method handles all the variables correctly and works for any given flight condition while the your approach is limited to one given Cl/AoA. Therefore for this particular case, speed change due to weight change, the polar method is the correct one.
And if want to disagree, please prove that with calculation.
Quote:
Originally Posted by Crumpp
What? Stop with the creepy weirdness.
I am sorry but Embry Riddle taught me to performance calculations in courses like ASCI 310 and ASCI 510.
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I quess that you have missed some lectures then or why I had to show the correct method and point out your errors here:
http://forums.ubi.com/eve/forums/a/t...6131040055/p/1