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Calculating gas turbine thermodynamic cycle using GateCycle TM software

Manh Duc Vu 1, *
Thang Huy Ha 2
Thang Trong Dao 1
Kien Trung Nguyen 1
  1. Military Technology Academy
  2. Electric Power University
Correspondence to: Manh Duc Vu, Military Technology Academy. Email: pvphuc@vnuhcm.edu.vn.
Volume & Issue: Vol. 20 No. K5 (2017) | Page No.: 30-36 | DOI: 10.32508/stdj.v20iK5.1156
Published: 2017-08-31

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Copyright The Author(s) 2023. This article is published with open access by Vietnam National University, Ho Chi Minh city, Vietnam. This article is distributed under the terms of the Creative Commons Attribution License (CC-BY 4.0) which permits any use, distribution, and reproduction in any medium, provided the original author(s) and the source are credited. 

Abstract

Gas turbine engines are widely used in aviation and naval ships for their compactness and high mobility. In Vietnam, the researches and investigations for this type of engine are less interested. In this paper, the authors present methods of modeling and calculating gas turbine thermodynamic cycle by using the General Electric software – GateCycleTM. The results can be used for the study of gas turbine engines and for engine operation.

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