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International Journal of Turbo & Jet-Engines

4.5 (402) · € 32.50 · En Stock

Objective 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. Topics Turbo and jet engines Theory and design of propagation of (advanced) jet aircraft Thermodynamics Combustion Behavior of materials at High temperatures Turbine and engine design Thrust vectoring or Jet-Engine-Steering in effecting improved Flight control Energy and environmental issue Stealth in Integrated Systems Design, including jet-engine inlets and exhausts Vectoring and safety in air, sea and land jet systems Article formats The journal welcomes scholarly research papers, invited review articles, and short communications

Engine Reliability and Supply Surfaces for Commercial Aircraft

NASA, Industry Advance Jet Engines and Sustainable Fuel

International Journal of Turbo and Jet Engines

Safe Flight: New Method Detects Onset of Destructive Oscillations

Sustainability, Free Full-Text

Efficient Compressor and Turbine Sealing in Aerospace

A new ductility exhaustion model for high

Multi-disciplinary conceptual design of future jet engine systems

7 Parts of Gas Turbine Engines and their Functions Explained

Turbo Jet Engine Research

International Gas Turbine Institute (IGTI) - ASME

empowering-gas-turbine-engineers, Engineering