Engine which can be estimated through statistical jet engine model has bypass ratio of 1.2 and maximum thrust at takeoff is 8000 Newton then what should be the design diameter for this engine. Consider a subsonic non after burning engine.

Propulsion and Fuel System Integration topics include: Propulsion selection, fuel system, jet engine and propeller engine integration. Propulsion system integration refers to the technology that combines propulsion systems with aircraft structures to meet an aircraft's mission. This includes combining engines, fuel systems, and exhaust systems.  Propulsion system integration involves aerodynamic, structural, and subsystem interfaces. These interfaces can include fuel, pneumatic, hydraulic, electrical, and control systems.  Propulsion system integration also ensures that the installed... Show more

Propulsion and Fuel System Integration topics include: Propulsion selection, fuel system, jet engine and propeller engine integration.

Propulsion system integration refers to the technology that combines propulsion systems with aircraft structures to meet an aircraft's mission. This includes combining engines, fuel systems, and exhaust systems. 
Propulsion system integration involves aerodynamic, structural, and subsystem interfaces. These interfaces can include fuel, pneumatic, hydraulic, electrical, and control systems. 
Propulsion system integration also ensures that the installed system meets or exceeds the expectations of the builder and customer. 

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