[1] Laveneziana L, Rosafio N, Salvadori S, Misul DA, Baratta M, Forno L, et al. Conjugate Heat Transfer Analysis of the Aero-Thermal Impact of Different Feeding Geometries for Internal Cooling in Lifetime Extension Processes for Heavy-Duty Gas Turbines. Energies. 2022;15(9):3022. DOI
https://doi.org/10.3390/en15093022
[2] da Graca Carvalho M, Coelho PJ. Heat transfer in gas turbine combustors. Journal of Thermophysics and Heat Transfer. 1989;3(2):123–31. DOI
https://doi.org/10.2514/3.138
[3] Kim KM, Yun N, Jeon YH, Lee DH, Cho HH, Kang S-H. Conjugated heat transfer and temperature distributions in a gas turbine combustion liner under base-load operation. Journal of Mechanical Science and Technology. 2010;24(9):1939–46. DOI
https://doi.org/10.1007/s12206-010-0625-8
[4] Lefebvre AH, Ballal DR, Taylor, Francis, Lefebvre AH, Ballal DR. Gas turbine combustion : alternative fuels and emissions. Third edition. ed. Boca Raton: Taylor & Francis; 2010. DOI
https://doi.org/10.1201/9781420086058
[5] Ahmet Topal SU, Altug Piskin. One-Dimensional Heat Transfer Analysis and Experimental Investigation of a Gas Turbine Combustor. International Symposium on Convective Heat and Mass Transfer; Turkey2014. DOI
http://dx.doi.org/10.1615/ICHMT.2014.IntSympConvHeatMassTransf.230
[6] Mattingly JD, Heiser WH, Boyer KM, Haven BA, Pratt DT. Aircraft engine design. Third edition ed. Reston, Virginia: American Institute of Aeronautics and Astronautics. DOI
https://doi.org/10.2514/5.9781624105173.0000.0000
[7] Sawyer JW, Japikse D. Sawyer's Gas turbine engineering handbook. 3rd ed. Norwalk, Conn., USA: Turbomachinery International Publications; 1985. 3 v : ill p. DOI
https://doi.org/10.1016/B978-0-7506-7846-9.X5000-7
[8] Shao C, Liu Y, Zhang Z, Lei F, Fu J. Fast Prediction Method of Combustion Chamber Parameters Based on Artificial Neural Network. Electronics. 2023;12(23):4774. DOI
https://doi.org/10.3390/electronics12234774
[9] Khosravian E. Numerical Investigation and Machine Learning Predictions for Enhanced Thermal Management in Pulsating Heat Pipes: Modeling Turbulent Flow and Heat Transfer Characteristics in Nuclear Applications. International Journal for Numerical Methods in Fluids. 2025;97(4):446–61. DOI
http://dx.doi.org/10.1002/fld.5358
[10] Deb K, Pratap A, Agarwal S, Meyarivan T. A fast and elitist multiobjective genetic algorithm: NSGA-II. IEEE Transactions on Evolutionary Computation. 2002;6(2):182–97. DOI
http://dx.doi.org/10.1109/4235.996017
[11] Conrado AC, Lacava PT, Carlos AL, Filho P, Física Dd, Sanches MdS, editors. BASIC DESIGN PRINCIPLES FOR GAS TURBINE COMBUSTOR, 2004.
[12] Mark CP, Selwyn A. Design and analysis of annular combustion chamber of a low bypass turbofan engine in a jet trainer aircraft. Propulsion and Power Research. 2016;5(2):97–107. DOI
https://doi.org/10.1016/j.jppr.2016.04.001
[13] Sitharam TG, Govindaraju L, SpringerLink. Theory of Elasticity. 1st 2021. ed. Singapore: Springer Singapore : Imprint: Springer; 2021. DOI
https://doi.org/10.1007/978-981-33-4650-5
[14] Glass DE, Dilley AD, Kelly HN, Langley Research C. Numerical analysis of convection/transpiration cooling. Hampton, Virginia: National Aeronautics and Space Administration, Langley Research Center; 1999. DOI
https://doi.org/10.2514/2.3666
[15] Pera RJ, Onat EA, Klees GW, Tjønneland EN, editors. A method to estimate weight and dimensions of aircraft gas turbine engines. Volume 1: Method of analysis1977.
[16] https://www.grc.nasa.gov/www/k-12/airplane/turbwt.html [
[17] Martins DAR. Off-Design Performance Prediction of the CFM56-3 Aircraft Engine: universidade de lisboa; 2015.
[18] Serbezov V. TURBOFAN ENGINE MODEL FOR ESTIMATION OF THE FUEL CONSUMPTION FOR COMPENSATION OF AUXILIARY ENERGY SUPPLY. 2011.
[19] https://www.gasturb.com/
[20] Habermehl S. Coefficient of thermal expansion and biaxial Young's modulus in Si-rich silicon nitride thin films. Journal of Vacuum Science & Technology A. 2018;36(2). DOI
https://doi.org/10.1116/1.5020432
