Right option is (a) Wf / W0 = 1 – (Wx / W0)
Best explanation: The fuel-fraction method is used to determine total fuel weight fraction.
According to which if there are x – number of mission phases in mission profile then the total fuel weight fraction is given by,
Wf / W0 = 1 – (Wx / W0)
Since, reserved fuel is not mentioned we can neglect it.