[1] Asgari, H., XiaoQi, C., Sainudiin, R. (2013). “Modelling and Simulation of Gas Turbines”. Modelling
Identification and Control, Vol. 20 , n. 3, pp.253-268.
[2] Novikov, Y. (2012). “Development of a High-Fidelity Transient Aerothermal Model For a Helicopter
Turboshaft Engine For Inlet Distortion And Engine Deterioration Simulations”. Master of Science in
Aerospace Engineering Dissertation, Middle East Technical University.
[3] Changduk, K. Park, J. (2004). ”Trannsient Performance Simulation of Propulsion System for CRW Type UAV
Using Simulink”. ICAS 2004.
4] منتدری، م ، رفرروادی فراهانی، م ی 1387 ، مدل سازی ر ش یه سازی لاملارد یکروی گاز هکایی وه مندکر طراضی سی ستم کنترل ]
107- سکخت ندریه وی المللی لالکم مهندسی داندگاه لالم ر رنعت ایران، لد 19 ، شماره 10 -ب رفسه 99
[5] Rahman, NU., Whidborne, JF. (2008). “A Numerical Investigation Into The Effect of Engine Bleed on Performance
of a Single-Spool Turbojet Engine” .Journal of Aerospace Engineering, Vol.222 , pp 939-
949.
[6] Martin, S., Wallace, I., and Bates, D.G. (2008). “Development and Validation of an Aero-Engine Simulation
Advanced Controller Design”. American Control Conference, 2008, pp. 2334-2339
[7] Martin, S. (2009). “Development and Validation of a Civil Aircraft Engine Simulation Model For Advanced
Controller Design”. PhD Dissertation Leicester University.
[8] Chiesa, S., Medici, G.,and Balbo, M. (2012). “Turbojet Analytical Model Development And Validation”. 28th
ICAS.
9] من صکری، ح ، مداهری، ک ی 1391 ، ش یه سازی لاملارد ضالت گذرای مکیکر یکروک ت در دررهای وات، وی ستمی کنفرانت ساتنه ]
مهندسی ماانی ، شیراز، داندگاه شیراز
[10] Ujam, A.J., Ifeacho, F.,and Anakudo, G. (2013). “Modeling Performance Characteristics of a Turbojet
Engine”. Journal of Manufacturing, Material and Mechanical Engineering Research, Vol.1 , n.1 ,
pp.1-16.
[11] Bettocchi, R., Pinelli, M., Spina, P. R., Venturini, M. and Burgio, M. (2004) “Set up of a Robust Neural
Network for Gas Turbine Simulation”, ASME Turbo Expo 2004, Vienna, Austria. Vol.4 , pp.543-
551.
[12] Walsh, PP., Fletcher, P.“Gas Turbine Performance”. Blackwell Science Publishing ,Inc. Ed 2. 2004.
[13] Cohen, H., Ragers, GFC., Saravanamuttoo, HIH. “Gas Turbine Theoury”. Longman Group. Ed 4. 1996.
[14] Burlamaqui Filho, F.A.C., Goes, L.C.S., Oliveira, A.B.V., Bosa, R.W., and Fernandes, G.S. (2012).
“Dynamic Modelling Nonlinear and Control System for a Turboshaft”. 12th Pan-American Congress
of Applied Mechanics, Port of Spain, Trinidad.
[15] Schur, F. (2013). “a Transient Model of a Turbofan Engine in Simulink”. Deutscher Luft- und Raumfahrt
Congress.
[16] GSP Development Team., (2013). “GSP 11 User Manual”. National Aerospace Laboratory (NLR),
www.gspteam.com.
[17] User Manual- MATLAB (R2014a).
[18] Sanghi, V., Lakshmanan, B.K. (2001). “Aerothermal Model for Real-Time Digital Simulation of a Mixed-
Flow Turbofan Engine”. Journal of Propultion and power, Vol.17 , n.3 ,629-635.
مجله
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