Right choice is (a) True
For explanation I would say: Relative airspeed acts as a shaping factor. Relative airspeed is given by \(\Big\{\frac{2u^3}{u^4+1}\Big\}\) where u is relative airspeed. The range equation in cruise method 1 is given by R1=\(\Big[\frac{V_{mdi}}{C}E_{max}\Big]\Big\{\frac{2u^3}{u^4+1}\Big\}\)lnω where V is true airspeed, C is specific fuel consumption, L is lift, D is drag, Emax is endurance, u is relative airspeed and ω is fuel ratio.