I am in my preliminary design course and was unable to access certain resources during the thanksgiving break, that equation is from Jan Roskam's text. You are correct about the inlet pressure recovery factor and I am consulting with my professor right now. Thank you very much for your help on...
Well, I am trying to create a graph of trust available vs. speed. The equation I am using is
T(avl) = T(tst)[1-0.35K(t)M*[1-(pressure loss)]]-550(P(extr)/U)
where T(avl)=thrust available
T(tst) = Uninstalled Thrust (23000lb for the V2522)
K(t)= constant
M = flight mach number
P(extr) =...
I am not positive, but I have been using Jan Roskam's texts on Aircraft Design in my prelim design class. It's a 9 part series and I'm wondering if any of the books have that information. If you haven't already, I would suggest taking a look at that. Hope that helps
Chester
I am trying to find out the pressure loss for the IAE V2522-A5 turbofan and am having a lot of trouble. Does anyone have this information or know where I could find it?
