Delete comment from: Elements Of Power
Hi LouG.
Yes I'm acutely aware of the altitude factor :-).
I identified it as an unknown and an assumption for the F-35A_H case, as a "Bowman configuration" 15k feet altitude assumption in Part 1. Aircraft selected for comparison were selected specifically because I had plots for 15k feet performance as well. In Part 1, I specifically note that the only thing ANYONE can conclude with certainty was the change in Bank Angle in a turn at constant speed and altitude. Everything that comes after is parametric exploration for understanding of the relevance of same. I'll link this part back to the other parts after I'm done with the series for clarity.
Thanks
May 22, 2013, 5:07:48 PM
Posted to The F-35 and the Infamous “Sustained G” Spec Change: Part 2