Based on first order statistical jet engine model, we have been given a task to design a subsonic non afterburning engine which is operating at maximum Mach number of 0.7. Evaluate the approximate length required to build this engine. Given thrust at takeoff is 9600 unit.

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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