[1] Zheng X., Zeng H., Wang B., et al., Numerical simulation method of surge experiments on gas turbine engines. Chinese Journal of Aeronautics, 2023, 36(3): 107–120.
[2] Yue K., Cheng L., Zhang T., et al., Numerical simulation of the aerodynamic influence of an aircraft on the hose-refueling system during aerial refueling operations. Aerospace Science and Technology, 2016, 49: 34–40.
[3] Tang T., Liu B., The genetic algorithm-radial basis function neural network to quickly predict aerodynamic performance of compressors. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 235(5): 537–552.
[4] Yang C., Wu H., Du J., et al., Full-engine simulation of micro gas turbine based on time-marching throughflow method. Applied Thermal Engineering, 2022, 217: 119213.
[5] Xu Y., Yan C., Piao Y., Analysis of discrepancies between 3-D coupled and uncoupled schemes based on CFD in full engine simulation. Aerospace Science and Technology, 2022, 131: 107978.
[6] Briones A.M., Caswell A.W., Rankin B.A., Fully coupled turbojet engine computational fluid dynamics simulations and cycle analyses along the equilibrium running line. Journal of Engineering for Gas Turbines and Power, 2021, 143(6): 061019.
[7] Jia Z., Tang H., Jin D., et al., Research on the volume-based fully coupled method of the multi-fidelity engine simulation. Aerospace Science and Technology, 2022, 123: 107429.
[8] Klein C., Reitenbach S., Schoenweitz D., et al., A fully coupled approach for the integration of 3D-CFD component simulation in overall engine performance analysis. ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, 2017, Paper No: GT2017-63591.
[9] Jia L., Chen Y., Cheng R., et al., Designing method of acceleration and deceleration control schedule for variable cycle engine. Chinese Journal of Aeronautics, 2021, 34(5): 27–38.
[10] Pang S., Li Q., Feng H., A hybrid onboard adaptive model for aero-engine parameter prediction. Aerospace Science and Technology, 2020, 105: 105951.
[11] Zhou X., Lu F., Huang J., Fault diagnosis based on measurement reconstruction of HPT exit pressure for turbofan engine. Chinese Journal of Aeronautics, 2019, 32(5): 1156–1170.
[12] Zhuang L., Xu G., Dong B., et al., Study on performance and mechanisms of a novel integrated model with power & thermal management system and turbofan engine. Applied Thermal Engineering, 2023, 219: 119481.
[13] Wang Z., Zhang J., Gao C., et al., Effect of air properties on a twin-shaft turbofan engine performance during start-up. Applied Thermal Engineering, 2023, 218: 119387.
[14] Hao X., Sun L., Chi J., et al., Off-design performance of 9f gas turbine based on gPROMs and BP neural network model. Journal of Thermal Science, 2022, 31(1): 261–272.
[15] Chen X., Chu W., Wang G., et al., Effect of span range of variable-camber inlet guide vane in an axial compressor. Aerospace Science and Technology, 2021, 116: 106836.
[16] Wei Z., Ni M., Gan X., et al., Generation of unsteady incoming wakes for wake/blade interaction. Aerospace Science and Technology, 2020, 106: 106127.
[17] Barsi D., Perrone A., Qu Y., et al., Compressor and turbine multidisciplinary design for highly efficient micro-gas turbine. Journal of Thermal Science, 2018, 27(3): 259–269.
[18] Pachidis V., Pilidis P., Texeira J., et al., A comparison of component zooming simulation strategies using streamline curvature. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2007, 221(1): 1–15.
[19] Pachidis V., Pilidis P., Templalexis I., et al., A de-coupled approach to component high-fidelity analysis using computational fluid dynamics. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2007, 221(1): 105–113.
[20] Pachidis V., Pilidis P., Talhouarn F., et al., A fully integrated approach to component zooming using computational fluid dynamics. Journal of Engineering for Gas Turbines and Power, 2004, 128(3): 579–584.
[21] Pachidis V., Pilidis P., Guindeuil G., et al., A partially integrated approach to component zooming using computational fluid dynamics. ASME Turbo Expo 2005: Power for Land, Sea, and Air, 2005, Paper No: GT2005-68457.
[22] Alexiou A., Tsalavoutas A., Introduction to gas turbine modelling with PROOSIS. Empresarios Agrupados Internacional (EAI) SA, Madrid Spain, 2011.
[23] Lytle J., Follen G., Naiman C., et al., 2001 numerical propulsion system simulation review. 2002, NASA Technical Reports, NASA/TM-2002-211197.
[24] Reed J.A., Afjeh A.A., Development of a prototype simulation executive with zooming in the numerical propulsion system simulation. 1995, NASA Technical Reports, NASA-CR-200613.
[25] Evans A., Follen G., Naiman C., et al., Numerical propulsion system simulation’s national cycle program. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-98-3113.
[26] John K.L., The numerical propulsion system simulation: An overview. 2000, NASA Technical Reports, NASA/TM-2000-209915.
[27] Guo L., Li G., Hu C., et al., Optimization of flow matching schemes for a heavy gas turbine burning syngas. Journal of Thermal Science, 2020, 29(5): 1292–1299.
[28] Templalexis I., Alexiou A., Pachidis V., et al., Direct coupling of a two-dimensional fan model in a turbofan engine performance simulation. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, 2016, Paper No: GT2016-56617.
[29] Xu Z., Li M., Tang H., et al., A multi-fidelity simulation method research on front variable area bypass injector of an adaptive cycle engine. Chinese Journal of Aeronautics, 2022, 35(4): 202–219.
[30] Turner M.G., Reed J.A., Ryder R., et al., Multi-fidelity simulation of a turbofan engine with results zoomed into mini-maps for a zero-d cycle simulation. ASME Turbo Expo 2004: Power for Land, Sea, and Air, 2004, Paper No: GT2004-53956.
[31] Claus R., Lavelle T., Townsend S., et al., Challenges in the development of a multi-fidelity, coupled component simulation of complex systems. 44th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit, 2008, AIAA 2008-4651.
[32] Claus R., Lavelle T., Townsend S., et al., Variable fidelity analysis of complete engine systems. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007, AIAA 2007-5042.
[33] Claus R., Townsend S., Lavelle T., et al., A case study of high fidelity engine system simulation. 42nd AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006, AIAA 2006-4971.
[34] Tang H., Chen M., Jin D., et al., High altitude low Reynolds number effect on the matching performance of a turbofan engine. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2013, 227(3): 455–466.
[35] Connolly J.W., Friedlander D.J., Kopasakis G., Computational fluid dynamics modeling of a supersonic nozzle and integration into a variable cycle engine model. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014, AIAA 2014-3687.
[36] Allison D.L., Alyanak E.J., Development of installed propulsion performance model for high-performance aircraft conceptual design. 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2014, AIAA 2014-2725.
[37] Song F., Zhou L., Wang Z., et al., Integration of high-fidelity model of forward variable area bypass injector into zero-dimensional variable cycle engine model. Chinese Journal of Aeronautics, 2021, 34(8): 1–15.
[38] Pilet J., Lecordix J.C., Garcia-Rosa N., et al., Towards a fully coupled component zooming approach in engine performance simulation. ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, 2011, Paper No: GT2011-46320.
[39] Xiang J., Schlüter J.U., Duan F., Study of KJ-66 micro gas turbine compressor: Steady and unsteady Reynolds-averaged Navier-Stokes approach. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231(5): 904–917.
[40] Schreckling K., Home built model turbines. Worcestershire, UK: Traplet Publications Ltd, 2005.
[41] Walsh P.P., Fletcher P., Gas turbine performance. John Wiley & Sons, 2004.
