Open Science Research Excellence

ICAPT 2021 : International Conference on Aircraft Propulsion Technology

New York, USA
December 9 - 10, 2021

Conference Code: 21US12ICAPT

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, OpenAIRE, BASE, WorldCAT, Sherpa/RoMEO, and other index databases. Impact Factor Indicators.

Special Journal Issues

ICAPT 2021 has teamed up with the Special Journal Issue on Aircraft Propulsion Technology. 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.

Important Dates

Abstracts/Full-Text Paper Submission Deadline   September 30, 2020
Notification of Acceptance/Rejection   October 15, 2020
Final Paper (Camera Ready) Submission & Early Bird Registration Deadline   November 11, 2021
Conference Dates   December 9 - 10, 2021

Important Notes

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 GUIDE before submitting your paper.

Selected Conference Papers

1) Design and Analysis of Annular Combustion Chamber for a Micro Turbojet Engine
Rashid Slaheldinn Elhaj Mohammed
2) 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
3) Integral Methods in the Determination of Temperature Fields of Cooled Blades of Gas Turbines
C. Ardil
4) Availability Analysis of a Power Plant by Computer Simulation
Mehmet Savsar
5) Computational Analysis of the Scaling Effects on the Performance of an Axial Compressor
Junting Xiang, Jörg Uwe Schlüter, Fei Duan
6) Substructure Method for Thermal-Stress Analysis of Liquid-Propellant Rocket Engine Combustion Chamber
Olga V. Korotkaya
7) Modeling of Temperature Fields of Gas Turbine Blades by Considering Heat Flow and Specified Temperature
C. Ardil
8) CFD Investigation of the Effects of Re-Entrant Combustion Chamber Geometry in a HSDI Diesel Engine
Raouf Mobasheri, Zhijun Peng
9) Numerical Study of Oxygen Enrichment on NO Pollution Spread in a Combustion Chamber
Zohreh Orshesh
10) Numerical Study on CO2 Pollution in an Ignition Chamber by Oxygen Enrichment
Zohreh Orshesh
11) Modeling And Analysis of Simple Open Cycle Gas Turbine Using Graph Networks
Naresh Yadav, I.A. Khan, Sandeep Grover
12) Operational- Economics Based Evaluation And Selection of A Power Plant Using Graph Theoretic Approach
Naresh Yadav, I.A. Khan, Sandeep Grover
13) Development of Effective Cooling Schemes of Gas Turbine Blades Based on Computer Simulation
Pasayev, C. Askerov, R. Sadiqov, C. Ardil

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