Reference77 articles.
1. Jaw, L.C., and J.D. Mattingly. 2009. Aircraft engine controls: Design, system analysis and health monitoring, AIAA, Inc., Virginia.
2. MacIsaak, B.D., and H.I.H. Saravanamutto. 1974. A comparison of analog, digital and hybrid computing techniques for simulation of gas turbine performance. ASME Paper No. 74-GT-127.
3. Walsh, P.P., and P. Fletcher .2002. Gas turbine performance, blackwell science, USA, 1998. In Two-spool, turbo-fan engine: (a) steady-state and dynamic mathematical models, ed. Lichtsinder, M., and Y. Levy, 20–37. Technion, Israel, TAE No. 903.
4. Khalid, S.J., and R.N. Hearne. 1980. Enhancing dynamic model fidelity for improved prediction of turbofan engine transient performance. AIAA 80–1083.
5. Lichtsinder, M., and Y. Levy. 2006. Jet engine model for control and real-time simulations. ASME Journal of Engineering for Gas Turbines and Power 128:745–753.
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Surge-Elimination Strategy for Aero-Engine Transient Control;Journal of Dynamic Systems, Measurement, and Control;2024-04-05