本杂志的主要目的和范围是帮助改进每一个单独的部件的研发和叠加分离结果，以获得集成系统，努力达到整体的先进设计和效益，通过集成：（a）物理、航空和隐身热力学在由集成支持的无人或载人原型飞行模拟中的应用。计算机仿真基于：（b）涡轮和喷气发动机的部件研发，（i i）机身，（i i i）头盔瞄准系统和弹药，基于：（c）预期的新项目任务，基于（d）涡轮和喷气发动机民用和军用领域的可靠性、耐用性、经济性、战术、战略和教育的改进。国际涡轮喷气发动机杂志致力于喷气式飞机传播理论和设计的前沿研究。它是一个国际出版机构，提供有关热力学、燃烧、高温下相关材料行为、涡轮和发动机设计、推力矢量控制和飞行控制以及能源和环境问题的工业和学术研究的新想法、见解和成果。
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.
* 请认真填写需求信息，学术顾问24小时内与您取得联系。
投稿咨询