The correct option is (a) 1.316 Vmd
For explanation: Brequet Range expression is given by R1 = \(\frac{V}{C}\frac{L}{D}\) ln ω where V is true airspeed, C is specific fuel consumption, L is lift, D is drag, and ω is fuel ratio. This Brequet Range expression comes in the cruise method 1. Brequet Range expression value is maximum at 1.316 Vmd.