International Journal of Turbo and Jet Engines

Aims & Scope

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.

View Aims & Scope

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Metrics & Ranking

Impact Factor

Year	Value
2025	0.9
2024	0.70

Journal Rank

Year	Value
2024	17458

Journal Citation Indicator

Year	Value
2024	244

SJR (SCImago Journal Rank)

Year	Value
2024	0.276

Quartile

Year	Value
2024	Q3

h-index

Year	Value
2024	28

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Abstracting & Indexing

Journal is indexed in leading academic databases, ensuring global visibility and accessibility of our peer-reviewed research.

• Scopus
• Google Scholar
• Web of Science

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Subjects & Keywords

Journal’s research areas, covering key disciplines and specialized sub-topics in Engineering, designed to support cutting-edge academic discovery.

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Most Cited Articles

The Most Cited Articles section features the journal's most impactful research, based on citation counts. These articles have been referenced frequently by other researchers, indicating their significant contribution to their respective fields.

• Semi-Inverse Method of Establishing Generalized Variational Principles for Fluid Mechanics With Emphasis on Turbomachinery Aerodynamics

  Citation: 196

  Authors: Ji-Huan

• Studies on Aerated-Liquid Atomization

  Citation: 67

  Authors: T.C., A.H.

• Fuel Performance Evaluation for the Solid-Fueled Ramjet

  Citation: 61

  Authors: A., D.W.

• A Review of Friction Damping of Turbine Blade Vibration

  Citation: 57

  Authors: Jerry H.

• Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview

  Citation: 45

  Authors: Narahari, R. K., Abhijit

• Numerical Studies on the Performance of Scramjet Combustor with Alternating Wedge-Shaped Strut Injector

  Citation: 33

  Authors: Gautam, K. M.

• The Effect of TiO2 on Engine Emissions for Gas Turbine engine Fueled with jatropha, butanol, Soya and Rapeseed Oil

  Citation: 32

  Authors: P., D. Raja, R., S., P., T.P. Prem, S., M. Rakesh

• A CFD Method for Axial Thrust Load Prediction of Centrifugal Compressors

  Citation: 32

  Authors: Zhen-Xue, Paul G.A.

• Exergetic, Exergoeconomic, Sustainability and Environmental Damage Cost Analyses of J85 Turbojet Engine with Afterburner

  Citation: 31

  Authors: Ozgur

• The Role of the Heat-up Period in Fuel Drop Evaporation

  Citation: 30

  Authors: J.S., A.H.

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