Originally posted by HoHun
Hi Badboy,
If my conclusions are self-evident because everyone knows that the Fw 190A outclimbs the Spitfire V, your conclusions are just as self-evident because everyone knows that the Spitfire V outturns the Fw 190A :-)
Absoulutely, which is why I wouldn’t normally have bothered to overlay the diagrams for those two particular aircraft, it was your comparison not mine :-) There are many other comparisons that aren’t so obvious, and even I have been surprised and delighted by the results, particularly when other aircraft configurations including the use of bombs, gun pods and flaps etc, are compared.
Your diagrams with the positive Ps graphs added makes an important step from a mere manoeuvrability diagram to a true energy manoeuvrability diagram, though I've got to admit you're right they're hard to read.
Yep, and I’ve had similar discussions with real fighter pilots who take the use of that type of diagram far more seriously than I do, including a weapons school instructor, and the conclusion seems to be that the form of diagram I am using now is an acceptable compromise for usefulness and simplicity
That's why I think a different way of graphing the energy information might improve the usefulness of such diagrams, and we should be looking for a different form to present the same information.
Yep, take a look at the alternative type of EM diagram shown below. With this sort of EM diagram, you don’t need a multitude of Ps curves because the angle of descent or climb can be read directly off the left hand vertical axis.

From that sort of diagram, you can read off the left vertical axis what angle of climb or descent can be achieved for any flight condition (in terms of the speed, load factor and turn radius), while the time for a 360° turn under those conditions can be read from the right hand axis. For example, for that diagram, if you entered a 6g turn at 200mph, you could turn 360° in under ten seconds with a turn radius of about 450ft, but to sustain it you would need an angle of descent of about 34° which I think is too steep to be a viable option.
That was the sort of EM diagram available during WWII, and I now produce both types automatically for every new aircraft I do, but I haven’t published any yet.
Badboy