What is the working principle of ‘fuel-fraction’ method?
(a) Division of mission profile into number of phases and finding individual phase fuel fraction
(b) Division of mission profile into 3 phases only
(c) Calculating fuel fraction for each stage
(d) Assuming any value for fuel fraction
This question was addressed to me in an interview for internship.
My question is taken from Conceptual Sketch Sizing in chapter Conceptual Sketch Sizing of Aircraft Design