RAM DRAG = GROSS THRUST NET Thrust = 12.5 0.88*12.5 = 1.5KN. "> RAM DRAG = GROSS THRUST NET Thrust = 12.5 0.88*12.5 = 1.5KN. ">
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Find the acceptable value of ram drag if Turbojet is designed to provide net thrust of 88% of gross thrust. Engine gross thrust is 12.5KN.

Aircraft Design Propulsion Jet-Engine Thrust Considerations and Turbojet Installed Thrust in Aircraft Design 1 week ago

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RAM DRAG = GROSS THRUST NET Thrust = 12.5 0.88*12.5 = 1.5KN.
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Posted on 04 Jul 2025, this text provides information on Aircraft Design related to Propulsion Jet-Engine Thrust Considerations and Turbojet Installed Thrust in Aircraft Design. Please note that while accuracy is prioritized, the data presented might not be entirely correct or up-to-date. This information is offered for general knowledge and informational purposes only, and should not be considered as a substitute for professional advice.

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