Right option is (d) \(\frac{\eta P}{V}\)=D+Wsinγ2+mV
Easiest explanation: The correct equation for longitudinal performance equation of motion is \(\frac{\eta P}{V}\)=D+Wsinγ2+mV where η is propeller efficiency, V is true airspeed, P is shaft power, D is propeller diameter, m is mass flow rate, W is weight.