The International Research Conference Aims and Objectives
The International Research Conference is a federated organization dedicated to bringing together a significant number of diverse scholarly events for presentation
within the conference program. Events will run over a span of time during the conference depending on the number and length of the presentations.
With its high quality, it provides an exceptional value for students, academics and industry researchers.
International Conference on Aerospace Propulsion and Combustion
aims to bring together leading academic scientists, researchers and research scholars to exchange and share their experiences and research results on all aspects of
Aerospace Propulsion and Combustion.
It also provides a premier interdisciplinary platform for researchers, practitioners and educators to present and discuss the most recent innovations,
trends, and concerns as well as practical challenges encountered and solutions adopted in the fields of Aerospace Propulsion and Combustion.
Call for Contributions
Prospective authors are kindly encouraged to contribute to and help shape the conference through submissions of their research abstracts, papers and e-posters.
Also, high quality research contributions describing original and unpublished results of conceptual, constructive, empirical, experimental, or
theoretical work in all areas of Aerospace Propulsion and Combustion are cordially invited for presentation at the conference.
The conference solicits contributions of abstracts, papers and e-posters that address themes and topics of the conference, including figures, tables and references of
novel research materials.
Guidelines for Authors
Please ensure your submission meets the conference's strict guidelines for accepting scholarly papers.
Downloadable versions of the check list for
Full-Text Papers and
Abstract Papers.
Please refer to the
Paper Submission Guideline,
Abstract Submission Guideline and
Author Information
before submitting your paper.
Conference Proceedings
All submitted conference papers will be blind peer reviewed by three competent reviewers.
The peer-reviewed conference proceedings are indexed in the Open Science Index,
Google Scholar,
Semantic Scholar,
Zenedo,
BASE,
WorldCAT,
Sherpa/RoMEO,
and other index databases. Impact Factor Indicators.
Special Journal Issues
19. International Conference on Aerospace Propulsion and Combustion has teamed up with the Special Journal Issue on
Aerospace Propulsion and Combustion.
A number of selected high-impact full text papers will also be considered for the special journal issues.
All submitted papers will have the opportunity to be considered for this Special Journal Issue.
The paper selection will be carried out during the peer review process as well as at the conference presentation stage.
Submitted papers must not be under consideration by any other journal or publication.
The final decision for paper selection will be made based on peer review reports by the Guest Editors and the Editor-in-Chief jointly.
Selected full-text papers will be published online free of charge.
Conference Sponsor and Exhibitor Opportunities
The Conference offers the opportunity to become a conference sponsor or exhibitor.
To participate as a sponsor or exhibitor, please download and complete the
Conference Sponsorship Request Form.
Selected Papers
-
Failure Analysis of a Fractured Control Pressure Tube from an Aircraft Engine
M. P. Valles-González, A. González Meije, A. Pastor Muro, M. García-Martínez, B. González Caballero
-
Hybrid Finite Element Analysis of Expansion Joints for Piping Systems in Aircraft Engine External Configurations and Nuclear Power Plants
Dong Wook Lee
-
Design and Analysis of Annular Combustion Chamber for a Micro Turbojet Engine
Rashid Slaheldinn Elhaj Mohammed
-
Wall Heat Flux Mapping in Liquid Rocket Combustion Chamber with Different Jet Impingement Angles
O. S. Pradeep, S. Vigneshwaran, K. Praveen Kumar, K. Jeyendran, V. R. Sanal Kumar
-
Integral Methods in the Determination of Temperature Fields of Cooled Blades of Gas Turbines
C. Ardil
-
Availability Analysis of a Power Plant by Computer Simulation
Mehmet Savsar
-
Computational Analysis of the Scaling Effects on the Performance of an Axial Compressor
Junting Xiang, Jörg Uwe Schlüter, Fei Duan
-
Substructure Method for Thermal-Stress Analysis of Liquid-Propellant Rocket Engine Combustion Chamber
Olga V. Korotkaya
-
Modeling of Temperature Fields of Gas Turbine Blades by Considering Heat Flow and Specified Temperature
C. Ardil
-
CFD Investigation of the Effects of Re-Entrant Combustion Chamber Geometry in a HSDI Diesel Engine
Raouf Mobasheri, Zhijun Peng
-
Numerical Study of Oxygen Enrichment on NO Pollution Spread in a Combustion Chamber
Zohreh Orshesh
-
Numerical Study on CO2 Pollution in an Ignition Chamber by Oxygen Enrichment
Zohreh Orshesh
-
Modeling And Analysis of Simple Open Cycle Gas Turbine Using Graph Networks
Naresh Yadav, I.A. Khan, Sandeep Grover
-
Operational- Economics Based Evaluation And Selection of A Power Plant Using Graph Theoretic Approach
Naresh Yadav, I.A. Khan, Sandeep Grover
-
Development of Effective Cooling Schemes of Gas Turbine Blades Based on Computer Simulation
Pasayev, A., C. Askerov, R. Sadiqov, C. Ardil
Digital Program consists of the e-proceedings book which is available online-only
and includes the conference communications (proceedings abstracts and papers).
Registered participants can access the digitally available conference
proceedings ( and certificates ) by visiting their profile pages.
Aerospace propulsion
Aircraft propulsion
Compressible flow with friction and heat
Engine thrust and performance parameters
Gas turbine engine cycle analysis
Aviation and uninhabited aerial vehicle propulsion system
Aircraft engine inlets and nozzles
Combustion chambers and afterburners
Axial compressor aerodynamics
Centrifugal compressor aerodynamics
Aero-thermo-dynamics of gas turbines
Aircraft engine component matching and off-design analysis
Chemical rocket and hypersonic propulsion
Aero-engine types
Reciprocating engines
Jet engines: turbojet, turbofan, propfan, turboprop, and ramjets
Engine parameters and performances
Jet fuel
Combustion chamber
From fuel to thrust: the energy conversion chain in jet propulsion
The simplest turbojet model
Thermal and mechanical limitations in jet engines
Jet engine auxiliaries: start-up, electrical, pneumatic and hydraulic services
Engine maintenance
Matching engines and aircraft
Aerodynamic drag and required propulsion power
Range and endurance
Take-off power
Effect of altitude, flight speed, and revolutions, on engine performances
Fuel tank inertization
Environmental impact
Aviation fuel consumption
Emissions and aircraft noise
Abstracts/Full-Text Paper Submission Deadline |
|
January 15, 2025 |
Notification of Acceptance/Rejection |
|
January 31, 2025 |
Final Paper (Camera Ready) Submission & Early Bird Registration Deadline |
|
March 11, 2025 |
Conference Dates |
|
April 03-04, 2025 |