Ram Drag of Turbojet given Gross Thrust evaluator uses Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet to evaluate the Ram Drag of Turbojet, Ram Drag of Turbojet given Gross Thrust formula is defined as the loss of thrust produced by a turbojet or turbofan engine caused by the increase of velocity of air entering the engine. Ram drag is the difference between gross thrust and net thrust. Ram Drag of Turbojet is denoted by Dram symbol.
How to evaluate Ram Drag of Turbojet given Gross Thrust using this online evaluator? To use this online evaluator for Ram Drag of Turbojet given Gross Thrust, enter Gross Thrust of Turbojet (TG) & Net Thrust of Turbojet (T) and hit the calculate button.