The 18th Israeli Symposium on Jet Engines and Gas Turbines - Call for Papers Registration deadline: September 15
For detailed information, please see the Supplementary Information below.
Cutting edge researches in theory and design of propagation of jet aircraft
New ideas crossing bridges between science and engineering
Special attention to environmental and safety issues
Top authors and reviewers
Internationally recognized editorial board
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.
Turbo and jet engines
Theory and design of propagation of (advanced) jet aircraft
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
Please submit your manuscript online to Editor-in-Chief or Deputy Editor – according to your topic
Publication for all papers accepted after peer reviewing procedure
In case of any problems editorial assistance will be provided
Contributions submitted to this journal must be written in clear and concise English. Only unpublished material can be accepted, and authors may not republish their paper in the same or similar form. The decision on the acceptance is taken after a peer-reviewing procedure
The journal makes no page charges
Galley proofs will be sent to all authors in due time with a request to carefully check them
After publication each author will receive a PDF file of the final version for private use only
Once your article is accepted you have the option to publish it open access
Our repository policy allows you to distribute 30 PDF copies of your published article to colleagues (the PDF has to include the information that it is an author's copy). Please also feel free to distribute the link to the online abstract
Effective 1st January 2016, authors from an institution affiliated with either the Association of Dutch Universities (VSNU), the Consortium of Swiss Academic Libraries or some UK libraries participating in the Jisc Collections SMP may publish primary research and review articles open access in any of De Gruyter's OnlineOpen journals at a discount of 90% of the APC price. For more information and to confirm whether your institution is eligible please see the following:
Original Editorial Board Members: E. Benstein, A. Brooks, Z. Goraj, R.D. Halverstadt, M.J. Ivanov, J. Sasion, Changduk Kong. C. Kuintzle, L. Larson, Shigeru Matso, D.P. Mishra, R.K. Mishra, M.V. Narasimhan, Youry A. Noznitsky, Noel Penny, C.R. Peterson, M.F. Platzer, A. Rao, Risshi S. Raj, Brian Spalding, W. Tabakoff, E. Tjonneland, P.J. Torvik, P.C. Tramm, Mitch Wolff, S. Yu, J. Zierep.
Professor IGOR LOBODA email@example.com INSTITUTO POLITCNICO NACIONAL Mexico Gas turbine design Systems and accessories of gas turbines Gas turbine diagnostics
Dr. JUAN LUIS PREZ RUIZ firstname.lastname@example.org INSTITUTO POLITCNICO NACIONAL Mexico Gas turbine condition monitoring and diagnostics Gas turbine performance simulation Data-driven and physics-based approaches for gas turbine diagnostics Artificial neural networks and machine learning techniques Pattern recognition
Fence height and clearance size on aerodynamic force,
Stiffness and damping of internal brush seals under different operating conditions
PROF. DR. HSIAO-WEI D. CHIANG , Taiwan email@example.com aeromechanics, aeroacoustics, rotor dynamics, turbomolecular pumps, dental air turbines, green energy, clean air to power, SOFC/MGT, micro power, microturbine generator system, hybrid vehicle, and ocean current turbine generation.
PROF. ONDER TURAN firstname.lastname@example.org Anadolu University, Turkey Propulsion, Exergy, Thermodynamics, Gas Turbines And Ecology Technology.
PROF. YASIN SOHRET email@example.com Sleyman Demirel University School of Civil Aviation Gas turbine engine measurements, Combustion and fuels, Energy and exergy analysis of thermal systems.
PROF. TOLGA BAKLACIO firstname.lastname@example.org Anadolu University, Turkey Optimization of Non-linear and Dynamic Systems in Aeronautics, Fuel Flow Rate Modeling of Turbofan Engines, Modeling of Exergy and Energy Efficiency and Sustainability Parameters of Aero-Engines, Aircraft Trajectory Prediction Models, Aircraft Emissions Index Estimation Modeling for Turbojet/Turbofan Aircraft, Thrust Models for Turbofan Engines, Artificial Neural Networks, Learning Algorithms, Deep Learning and Extreme Learning Techniques, Genetic Algorithms, Ant Colony Optimization, Particle Swarm Optimization, Evolutionary Algorithms, Stochastic Algorithms, Simulated Annealing
Prof. Dr.S.Thanigaiarasu email@example.com, firstname.lastname@example.org Anna UniversityChennai, Tamilnadu India High Speed Jets, Propulsion Aerodynamics Jet Acoustics Heat transfer Computational fluid dynamics
Prof. S.Elangovan email@example.com Bharath Institute of Higher Education and Research, Chennai-73, INDIA Jet Mixing, Passive Control Of Jets, Bluff Body Aerodynamics
Dr. Valeriu Dragan firstname.lastname@example.org INCDT Comoti,, Bucuresti (Romania) Centrifugal compressor design, CFD and testing Axial compressors and fan design, CFD and testing Surge and Stall in compressors and fans Design optimization methods and practices (Genetic Algorithms, Artificial Neural Networks, Adjoint Method) Radial turbine design, CFD and testing Generic CFD of aviation components
Dr. Chong Zhong email@example.com The University of Akron, Akron, OH fluid dynamics analysis, lubrication/fuel system modeling (FEA&CFD), non-contact measurement systems design /calibration /testing, signal acquisition/processing.
Dr. Hai Zhang firstname.lastname@example.org College of Power and Energy Engineering, Harbin Engineering University, Harbin, China Turbomachinery sealing technology Two-phase flow in turbomachinery MIPCC technique Water Ingestion Wet compression Spent fuel reprocessing
Dr. D. Ragni D.Ragni@tudelft.nl Delft University of Technology, Netherlands Aerodynamics Aeroacoustics Aerospace Engineering Mechanincal Engineering
Prof. Dr. S. Jeyakumar email@example.com Kalasalingam Academy of Research and Education Krishnankoil, India High-speed flow mixing and combustion, Supersonic combustion, Dual combustion ramjet engine, Flow diagnostics, Ramjet and scramjet engine flow analysis, Aero acoustics, Performance analysis of jet engines.
Dr. D. Crunteanu firstname.lastname@example.org Politechnika University of Bucharest, Romania Gas Dynamics, Combustion theory and numerical methods, Combustion with shock waves Fundamentals of Aero-Thermochemistry Turbomachinery Air breathing engines for aircraft, Advanced mathematics for engineers
Prof. Dr Jun Hashimoto, email@example.com Faculty of Science and Technology, Oita University, JapanTopics Premixed Combustion, non-Premixed Combustion, Turbulent Combustion Combustion Characteristics of Conventional and Alternative Fuels
Dr. Ali Dinc, firstname.lastname@example.org College of Engineering and Technology, American University of the Middle East, Kuwait Jet engines Unmanned Aerial Vehicles UAV preliminary design and sizing, Turbofan, turbojet turboprop engine performances Gas turbine cycle analysis NOx emission Global warming potential Generic algorithm optimization
Dr. Baofeng Tu email@example.com College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics Nanjing, China Fluid mechanics Aeroengine aerodynamics Turbomachinery aerodynamics
Prof. Xinjun Wang firstname.lastname@example.org Institute of Turbomachinery, Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Xian Jiatong University, Xian, China Turbomachinery Heat transfer Fluid dynamics
Prof. Kazhan email@example.com NAU, Kyiv, Ukraine Environment Engineering Civil Engineering Energy and Environment issue Entropy Optimization Airport Environmental Issues Aircraft Noise Airport environmental noise mapping and forecasting
Dr. Vivek Sanghi firstname.lastname@example.org Consultant and Visiting Professor Bangalore, India Cycle analyses of aero engines Thermodynamic modeling and performance prediction (steady state and transient) of aero engines Modeling engine starting and shut down phases Novel/Futuristic engine concept and their impact on system performance. Engine cycle selection/ Engine cycle optimization/Engine-Aircraft performance matching for a given mission application (or for given requirements) Technology impact forecasting Analysis of engine test results, fine tuning simulation models to match test results. Engine health monitoring (condition trend monitoring), fault analysis, diagnostics and prognostics Real time engine simulations and their use in control system development, testing and verification. Preliminary design of aero engine/ Engine gas flow path sizing
Prof. Antonio Davis email@example.com Int. Institute for Aerospace Engineering and Management, Jain University, Bangalore, India Aircraft Propulsion, Heat Transfer, Computational Fluid Dynamics
Dr. Lei Sun firstname.lastname@example.org Beijing University of Aeronautics and Astronautics Gas turbine/Aero engine combustor and combustion Atomizer Atomization and spray
Prof. Yepifanov Sergiy Yepif_khai@ukr.net Kharkov National Aerospace University, Ukraine Gas turbines and piston engines theory Design, strength and dynamics Cooling system design Automatic control, diagnostics and health monitoring Life time analysis
Dr. Chen Jie email@example.com College of Energy and Power Engineering Nanjing University of Aeronautics and Astronautics Compressor Aerodynamic Design, Mixed-flow Compressor, Radial Compressor, Blade Modeling Method