Published Paper Details:

The Mini turbine engine is an fuel combustion Engine which uses a Brayton cycle to run the cycles of the engine, in this specific scenario the Turbocharger of an IC engine has been used in a way so that it can optimally run The Brayton Cycle. The turbocharger is a very useful accessory of the IC engine which increases the efficiency of the engine by providing forced induction into the engine without actually depriving the engine performance of its own energy like in the case of a Supercharger. The Compressor (The cold side) and The Turbine (The hot side), of a Turbocharger are connected within which a combustion chamber is provided to sufficiently run The Brayton cycle. The Main aim and scope of this paper is to superimpose separated results to get integrated systems seek to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by artificial intelligence and Computer Simulations based on: (b) Component R&D of Turbo and Jet-Engines, Airframe, Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) improved reliability, efficiency, economics, tactics, strategies and education in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication fragment for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control stabilizers as well as energy and environmental issues.