Centrifugal Force in Accelerated Flight evaluator uses Centrifugal Force = Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle) to evaluate the Centrifugal Force, The Centrifugal Force in Accelerated Flight is a fictitious force that appears to act on objects moving in a circular path. It arises due to inertia and is perceived by an observer in the rotating frame of reference, this force acts perpendicular to the direction of the velocity vector. Centrifugal Force is denoted by Fc symbol.
How to evaluate Centrifugal Force in Accelerated Flight using this online evaluator? To use this online evaluator for Centrifugal Force in Accelerated Flight, enter Lift Force (FL), Thrust (T), Thrust Angle (σT), Mass of Aircraft (m) & Flight Path Angle (γ) and hit the calculate button.