The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving 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 integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, 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 organ 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 as well as energy and environmental issues.

本雜志的主要目的和范圍是幫助改進每一個單獨的部件的研發和疊加分離結果，以獲得集成系統，努力達到整體的先進設計和效益，通過集成：（a）物理、航空和隱身熱力學在由集成支持的無人或載人原型飛行模擬中的應用。計算機仿真基于：（b）渦輪和噴氣發動機的部件研發，（i i）機身，（i i i）頭盔瞄準系統和彈藥，基于：（c）預期的新項目任務，基于（d）渦輪和噴氣發動機民用和軍用領域的可靠性、耐用性、經濟性、戰術、戰略和教育的改進。國際渦輪噴氣發動機雜志致力于噴氣式飛機傳播理論和設計的前沿研究。它是一個國際出版機構，提供有關熱力學、燃燒、高溫下相關材料行為、渦輪和發動機設計、推力矢量控制和飛行控制以及能源和環境問題的工業和學術研究的新想法、見解和成果。