How to Calculate Drag in Accelerated Flight?
Drag in Accelerated Flight calculator uses Drag Force = Thrust*cos(Thrust Angle)-Mass of Aircraft*[g]*sin(Flight Path Angle)-Mass of Aircraft*Acceleration to calculate the Drag Force, The Drag in Accelerated Flight is a function of thrust, weight, thrust angle, flight path angle, and acceleration of aircraft. Drag Force is denoted by FD symbol.
How to calculate Drag in Accelerated Flight using this online calculator? To use this online calculator for Drag in Accelerated Flight, enter Thrust (T), Thrust Angle (σT), Mass of Aircraft (m), Flight Path Angle (γ) & Acceleration (a) and hit the calculate button. Here is how the Drag in Accelerated Flight calculation can be explained with given input values -> 80.04298 = 700*cos(0.034)-20*[g]*sin(0.062)-20*30.37.