BIGGEST obstacle of CURRENT ENGINE design. For best Thrust and efficiency it is desirable to use STOICHIOMETRIC air fuel ratio of 15:1. However, this generated tremendous HIGH temperatures. Such high temperatures are beyond the limits of materials used for Turbine.

"> BIGGEST obstacle of CURRENT ENGINE design. For best Thrust and efficiency it is desirable to use STOICHIOMETRIC air fuel ratio of 15:1. However, this generated tremendous HIGH temperatures. Such high temperatures are beyond the limits of materials used for Turbine.

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What is the limitation of current engine design?

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

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Turbine inlet temperature is one of the BIGGEST obstacle of CURRENT ENGINE design. For best Thrust and efficiency it is desirable to use STOICHIOMETRIC air fuel ratio of 15:1. However, this generated tremendous HIGH temperatures. Such high temperatures are beyond the limits of materials used for Turbine.

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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