- Agrawal, R.K. A Generalized Mathematical Model to Estimate Gas Turbine Starting Characteristics ASME Paper. In Turbo Expo: Power for Land, Sea, and Air; American Society of Mechanical Engineers: New York, NY, USA, 1980; No. 81-GT-202.
Paper not yet in RePEc: Add citation now
- Asgari, H.; Chen, X.; Sainudiin, R.; Morini, M.; Pinelli, M.; Spina, P.R.; Venturini, M. Modeling and simulation of the start-up operation of a heavy-duty gas turbine by using NARX models. In Turbo Expo: Power for Land, Sea, and Air; American Society of Mechanical Engineers: New York, NY, USA, 2014; Volume 45653, p. V03AT21A003.
Paper not yet in RePEc: Add citation now
- Asgari, H.; Chen, X.Q.; Morini, M.; Pinelli, M.; Sainudiin, R.; Spina, P.R.; Venturini, M. NARX models for simulation of the start-up operation of a single-shaft gas turbine. Appl. Therm. Eng. 2016, 93, 368â376. [CrossRef]
Paper not yet in RePEc: Add citation now
- Bahlawan, H.; Morini, M.; Pinelli, M.; Spina, P.R.; Venturini, M. Development of reliable narx models of gas turbine cold, warm and hot start-up. In Turbo Expo: Power for Land, Sea, and Air; American Society of Mechanical Engineers: New York, NY, USA; Charlotte, NC, USA, 2017; Volume 50961, p. V009T27A007.
Paper not yet in RePEc: Add citation now
- Braig, W.; Schulte, H.; Riegler, C. Comparative Analysis of the Windmilling Performance of Turbojet and Turbofan Engines. J. Propuls. Power 1999, 15, 326â333. [CrossRef]
Paper not yet in RePEc: Add citation now
- Bretschneider, S.; Reed, J. Modeling of Start-Up from Engine-Off Conditions Using High Fidelity Turbofan Engine Simulations. J. Eng. Gas Turbines Power 2016, 138, 051201-1â051201-6. [CrossRef]
Paper not yet in RePEc: Add citation now
- Chappell, M.A.; McLaughlin, P.W. Approach to Modeling Continuous Turbine Engine Operation from Startup to Shutdown. J. Propuls. Power 1993, 9, 466â471. [CrossRef]
Paper not yet in RePEc: Add citation now
- Davis, J.B.; Pollak, R.R. Criteria for Optimizing Starting Cycles for High Performance Fighter Engines. In Proceedings of the 19th Joint Propulsion Conference, Seattle, WA, USA, 27â29 June 1983. AIAA-83-1127.
Paper not yet in RePEc: Add citation now
- Erario, M.L.; De Giorgi, M.G.; Przysowa, R. Model-Based Dynamic Performance Simulation of a Microturbine Using Flight Test Data. Aerospace 2022, 9, 60. [CrossRef]
Paper not yet in RePEc: Add citation now
- Failer, L.; Richter, T. A parallel Newton multigrid framework for monolithic fluid-structure interactions. J. Sci. Comput. 2020, 82, 28. [CrossRef]
Paper not yet in RePEc: Add citation now
- Fentaye, A.D.; Gilani, S.I.U.H.; Baheta, A.T. Gas turbine gas path diagnostics: A review. MATEC Web Conf. 2016, 74, 00005. [CrossRef]
Paper not yet in RePEc: Add citation now
- Flack, R.D. Analysis and Matching of Gas Turbine Components. Int. J. Turbo Jet Engines 1990, 7, 217â226. [CrossRef]
Paper not yet in RePEc: Add citation now
- Ghaffari, A.; Akhgari, R.; Abbasi, E. Modeling and Simulation of MGT-70 Gas Turbine start-up procedure. Amirkabir J. Mech. Eng. 2017, 49, 363â370.
Paper not yet in RePEc: Add citation now
Guan, J.; Lv, X.; Spataru, C.; Weng, Y. Experimental and numerical study on self-sustaining performance of a 30-kW micro gas turbine generator system during startup process. Energy 2021, 236, 121468. [CrossRef]
- Jafari, S.; Miran Fashandi, S.A.; Nikolaidis, T. Modeling and control of the starter motor and start-up phase for gas turbines. Electronics 2019, 8, 363. [CrossRef]
Paper not yet in RePEc: Add citation now
- Kim, J.H.; Song, T.W. Dynamic Simulation of Full Startup Procedure of Heavy-Duty Gas Turbines. J. Eng. Gas Turbines Power 2002, 124, 510â516. [CrossRef]
Paper not yet in RePEc: Add citation now
- Klemetsdal, Ã.; Moncorgé, A.; Møyner, O.; Lie, K.A. A numerical study of the additive Schwarz preconditioned exact Newton method (ASPEN) as a nonlinear preconditioner for immiscible and compositional porous media flow. Comput. Geosci. 2022, 26, 1045â1063. [CrossRef] Sustainability 2023, 15, 3468 25 of 25
Paper not yet in RePEc: Add citation now
- Mathioudakis, K.; Politis, E.; Stamatis, A. A computer model as an educational tool for gas turbine performance. Int. J. Mech. Eng. Educ. 1999, 27, 114â125. [CrossRef]
Paper not yet in RePEc: Add citation now
- Mehrpanahi, A.; Hamidavi, A.; Ghorbanifar, A. A novel dynamic modeling of an industrial gas turbine using condition monitoring data. Appl. Therm. Eng. 2018, 143, 507â520. [CrossRef]
Paper not yet in RePEc: Add citation now
- Nannarone, A.; Klein, S.A. Start-Up Optimization of a CCGT Power Station Using Model-Based Gas Turbine Control. J. Eng. Gas Turbines Power 2019, 141, 041018. [CrossRef]
Paper not yet in RePEc: Add citation now
- Owen, A.K.; Daugherty, A.; Garrard, D.; Reynolds, H.C.; Wright, R.D. A Parametric Starting Study of an Axial-Centrifugal Gas Turbine Engine Using a One-Dimensional Dynamic Engine Model and Comparisons to Experimental Results: Part IâModel Development and Facility Description. J. Eng. Gas Turbines Power 1999, 121, 377â383. [CrossRef]
Paper not yet in RePEc: Add citation now
- Owen, A.K.; Daugherty, A.; Garrard, D.; Reynolds, H.C.; Wright, R.D. A Parametric Starting Study of an Axial-Centrifugal Gas Turbine Engine Using a One-Dimensional Dynamic Engine Model and Comparisons to Experimental Results: Part IIâSimulation Calibration and Trade-Off Study. J. Eng. Gas Turbines Power 1999, 121, 384â393. [CrossRef]
Paper not yet in RePEc: Add citation now
- Pakanati, S.; Sampath, R.; Irani, R.; Plybon, R.; Anderson, B. High Fidelity Engine Performance Models for Windmill Relight Predictions. In Proceedings of the Joint Propulsion Conference & Exhibit, Sacramento, CA, USA, 9â12 July 2006. AIAA 2006-4970.
Paper not yet in RePEc: Add citation now
Park, Y.; Choi, M.; Choi, G. Fault detection of industrial large-scale gas turbine for fuel distribution characteristics in start-up procedure using artificial neural network method. Energy 2022, 251, 123877. [CrossRef]
Qian, Y.; Ye, Z.; Zhang, H. Impact of Modeling Simplifications on Lightning Strike Simulation for Aeroengine. Math. Probl. Eng. 2019, 2019, 5176560. [CrossRef]
Qin, H.; Zhao, J.; Ren, L.; Li, B.; Li, Z. Performance Degradation Evaluation of Low Bypass Ratio Turbofan Engine Based on Flight Data. Sustainability 2022, 14, 8052. [CrossRef]
Ren, L.; Qin, H.; Xie, Z.; Xie, J.; Li, B. A Thermodynamics-Oriented and Neural Network-Based Hybrid Model for Military Turbofan Engines. Sustainability 2022, 14, 6373. [CrossRef]
- Riegler, C.; Bauer, M.; Schulte, H. Validation of a Mixed Flow Turbofan Performance Model in the Sub-Idle Operating Range. In Turbo Expo: Power for Land, Sea, and Air; American Society of Mechanical Engineers: New York, NY, USA, 2003; GT2003-38223.
Paper not yet in RePEc: Add citation now
Rossi, I.; Sorce, A.; Traverso, A. Gas turbine combined cycle start-up and stress evaluation: A simplified dynamic approach. Appl. Energy 2017, 190, 880â890. [CrossRef]
- Sheng, H.; Chen, Q.; Li, J.; Jiang, W.; Wang, Z.; Liu, Z.; Zhang, T.; Liu, Y. Research on dynamic modeling and performance analysis of helicopter turboshaft engineâs start-up process. Aerosp. Sci. Technol. 2020, 106, 106097. [CrossRef]
Paper not yet in RePEc: Add citation now
- Topel, M.; Nilsson, Ã
.; Jöcker, M.; Laumert, B. Investigation into the thermal limitations of steam turbines during start-up operation. J. Eng. Gas Turbines Power 2018, 140, 012603. [CrossRef]
Paper not yet in RePEc: Add citation now
- Wang, C.; Yu, H.; Wang, J.; Liu, T. Bias analysis of parameter estimator based on Gauss-Newton method applied to ultra-wideband positioning. Appl. Sci. 2019, 10, 273. [CrossRef]
Paper not yet in RePEc: Add citation now
- Wu, Y.; Liu, B.; Zhang, H.; Zhu, K.; Kong, B.; Guo, J.; Li, F. Accuracy and efficient solution of helical coiled once-through steam generator model using JFNK method. Ann. Nucl. Energy 2021, 159, 108290. [CrossRef]
Paper not yet in RePEc: Add citation now
- Xu, P.; Roosta, F.; Mahoney, M.W. Newton-type methods for non-convex optimization under inexact Hessian information. Math. Program. 2020, 184, 35â70. [CrossRef]
Paper not yet in RePEc: Add citation now
Ying, Y.; Cao, Y.; Li, S.; Li, J. Nonlinear steady-state model based gas turbine health status estimation approach with improved particle swarm optimization algorithm. Math. Probl. Eng. 2015, 2015, 940757. [CrossRef] Sustainability 2023, 15, 3468 24 of 25
- Yuan, G.; Sheng, Z.; Wang, B.; Hu, W.; Li, C. The global convergence of a modified BFGS method for nonconvex functions. J. Comput. Appl. Math. 2018, 327, 274â294. [CrossRef] Disclaimer/Publisherâs Note: The statements, opinions and data contained in all publications are solely those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). MDPI and/or the editor(s) disclaim responsibility for any injury to people or property resulting from any ideas, methods, instructions or products referred to in the content.
Paper not yet in RePEc: Add citation now
- Zhou, W.X. Research on Object-Oriented Modeling and Simulation for Aeroengine and Control System. Ph.D. Thesis, Nanjing University of Aeronautics and Astronautics, Nanjing, China, 2006. (In Chinese)
Paper not yet in RePEc: Add citation now
- Zhou, W.X.; Huang, J.Q. Development of Component-Level Startup Model for a Turbofan Engine. J. Aerosp. Power 2006, 21, 248â253. (In Chinese)
Paper not yet in RePEc: Add citation now