swampyankee
Chief Master Sergeant
- 4,031
- Jun 25, 2013
I'd be very leery of all those posted lift coefficients. It's fairly rare for airfoils to get no-flaps lift coefficients quite that high except for some fairly special cases, like the high-lift Liebeck airfoils (which generally suck otherwise). See, for example, Abbot & von Doenhoff, Summary of Airfoil Data, Summary of Airfoil Data - NASA Technical Reports Server (NTRS)Okay, I was looking at the figures cited from America's Hundred Thousand, which I've put into an Excel sheet (then turned that into a screen-cap)
View attachment 630207
The red stuff was things I either know are wrong or strongly suspect, the gray item was something I was just unsure of: The P-61B's wing area is 662.36 square feet and, while I'm unsure the exact C/L for the P-51, I've heard some sources that listed numbers lower (1.5). I'm curious if anybody has more accurate data on the coefficient of lift figures for the aircraft in question since I have doubts as to the accuracy of the source.
The wing-area for the P-51 seems to vary a bit from 233 to 235.7 or so. I'm not sure why there are variations in this area.
Thanks