Drag for Level and Unaccelerated Flight evaluator uses Drag Force = Thrust*cos(Thrust Angle) to evaluate the Drag Force, The Drag for Level and Unaccelerated Flight seems to imply a relationship between the drag force and the thrust of an aircraft at a certain thrust angle, the aircraft's thrust from its engines must overcome this drag to maintain a constant velocity. Drag Force is denoted by FD symbol.
How to evaluate Drag for Level and Unaccelerated Flight using this online evaluator? To use this online evaluator for Drag for Level and Unaccelerated Flight, enter Thrust (T) & Thrust Angle (σT) and hit the calculate button.