How to Calculate Drag in an accelerated flight?
Drag in an accelerated flight calculator uses Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) to calculate the Drag Force, The Drag in an accelerated flight is a function of thrust, weight, thrust angle, flight path angle, and acceleration of aircraft. Drag Force and is denoted by F_{D symbol.
How to calculate Drag in an accelerated flight using this online calculator? To use this online calculator for Drag in an accelerated flight, enter Thrust of an aircraft (T), Thrust angle (αT), Mass (m), Flight path angle (θ) and Acceleration (a) and hit the calculate button. Here is how the Drag in an accelerated flight calculation can be explained with given input values -> -337.626361 = (100*cos(2.00535228295826))-(35.45*[g]*(sin(2.00535228295826)))-(35.45*12).}