FLOW rate, exhaust velocity ETC. A typical aircraft thrust is nothing but the CHANGE in momentum. And hence, it will be affected by mass flow rate.

"> FLOW rate, exhaust velocity ETC. A typical aircraft thrust is nothing but the CHANGE in momentum. And hence, it will be affected by mass flow rate.

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Thrust generated by an engine is proportional to mass flow rate.

Aircraft Design Propulsion Jet-Engine Thrust Considerations and Turbojet Installed Thrust in Aircraft Design 2 weeks ago

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Thrust is nothing but the propulsive force which is used to accelerate aircraft. It will be used to provide forward motion. Thrust depends upon number of factors including mass FLOW rate, exhaust velocity ETC. A typical aircraft thrust is nothing but the CHANGE in momentum. And hence, it will be affected by mass flow rate.

Posted on 30 Jun 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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