Let’s consider our aircraft has to generate thrust of 150KN during cruise. If at the cruise thrust loading is 0.86 then, at which value of Lift our aircraft is flying?
(a) 174.4KN
(b) 450KN
(c) 100N
(d) 174N
I have been asked this question in a job interview.
This is a very interesting question from Flight Mechanics in portion Performance and Flight Mechanics of Aircraft Design