[1] Han, Je-Chin, Dutta, Sandip, and Ekkad, Srinath. Gas turbine heat transfer and cooling technology. CRC Press, 2012.
[2] Rolls Royce, plc. The jet engine. McGraw-Hill, 1986.
[3] Padture,NitinP,Gell,Maurice,andJordan,EricH. Thermal barrier coatings for gas-turbine engine applications. Science, 296(5566):280–284, 2002.
[4] Fang, X, Tang, J, Jordan, E, and Murphy, KD. Crack inducedvibrationlocalizationinsimplifiedbladed-diskstructures. Journal of sound and vibration, 291(1-2):395–418, 2006.
[5] Zhou, Shui-Ting, Chiu, Yi-Jui, Yu, Guo-Fei, Yang, ChiaHao, Huang, Hong-Wu, and Jian, Sheng-Rui. An assumed mode method and finite element method investigation of the coupled vibration in a flexible-disk rotor system with lacing wires. Journal of Mechanical Science and Technology, 31(2):577–586, 2017.
رﺋﯿﺴ،اﺣﺴﺎنوﺿﯿﺎﯾﯽ راد،ﺳﻌﯿﺪ. ﺑﺮرﺳﺗﺤﻘﯿﻘﺎتاﻧﺠﺎمﺷﺪهدرزﻣﯿﻨﻪ [۶]
. ١٣٩۴،٣٨ – ٢۵:(٨)۴، ﻃﺮاﺣﺳﯿﺴﺘﻢدﯾﺴوﭘﺮه.ﺻﻮتوارﺗﻌﺎش
[7] Rahimi, Mohammad and Ziaei-Rad, Saeed. Uncertainty treatment in forced response calculation of mistuned bladed disk. Mathematics and Computers in Simulation, 80(8):1746–1757, 2010.
[8] Salhi, Bendali, Lardies, Joseph, and Berthillier, Marc. Identification of modal parameters and aeroelastic coefficients in bladed disk assemblies. Mechanical Systems and Signal Processing, 23(6):1894–1908, 2009.
[9] Yan, YJ, Cui, PL, and Hao, HN. Vibration mechanism of a mistuned bladed-disk. Journal of sound and vibration, 317(1-2):294–307, 2008.
[10] Cha, D and Sinha, A. Statistics of responses ofa mistuned and frictionally damped bladed disk assembly subjected to white noise and narrow band excitations. Probabilistic Engineering Mechanics, 21(4):384–396, 2006.
[11] Ewins, D J_. The effects of detuning upon the forced vibrations of bladed disks. Journal of Sound and Vibration, 9(1):65–79, 1969.
[12] Wei, S-T and Pierre, C. Localization phenomena in mistuned assemblies with cyclic symmetry part i: free vibrations. Journal of Vibration, Acoustics, Stress, and Reliability in Design, 110(4):429–438, 1988.
[13] Kuang, JH and Huang, BW. The effect of blade crack on mode localization in rotating bladed disks. Journal of sound and vibration, 227(1):85–103, 1999.
[14] Castanier, Matthew P and Pierre, Christophe. Modeling and analysis of mistuned bladed disk vibration: current status and emerging directions. Journal of Propulsion and Power, 22(2):384–396, 2006.
[15] Huang, Bo-Wun and Kuang, Jao-Hwa. Variation in the stability of a rotating blade disk with a local crack defect. Journal of Sound and Vibration, 294(3):486–502, 2006.
[16] Dowell, Earl H. A modern course in aeroelasticity, vol. 217. Springer, 2014.
[17] Naudascher,E.andRockwell,D. Flow-InducedVibrations: An Engineering Guide. Dover Civil and Mechanical Engineering. Dover Publications, 2012.
[18] Walsh, Philip P and Fletcher, Paul. Gas turbine performance. John Wiley & Sons, 2004.
[19] Chatterjee, Animesh and Kotambkar, Mangesh S. Modal characteristics of turbine blade packets under lacing wire damage induced mistuning. Journal of Sound and Vibration, 343:49–70, 2015. ﺳﻤﻮات،ﺑﻬﻨﻮشورﻫ،ﻋﺒﺎس. ﺑﺮرﺳﺗﺎﺛﯿﺮﺳﯿﻢﻫﺎیﻣﺴﺘﻬﻠﮐﻨﻨﺪهﺑﺮ [٢٠] ارﺗﻌﺎﺷﺎتﭘﺮهﻫﺎیﻣﺘﺤﺮکردﯾﻒآﺧﺮﺗﻮرﺑﯿﻦﺑﺨﺎرﻧﯿﺮوﮔﺎهراﻣﯿﻦاﻫﻮاز.ﺻﻮت . ١٣٩۵،٣۴ – ٢۵:(١٠)۵،وارﺗﻌﺎش [21]
Mazanoglu, Kemal and Guler, Serkan. Flap-wise and chord-wise vibrations of axially functionally graded tapered beams rotating around a hub. Mechanical Systems and Signal Processing, 89:97–107, 2017.
[22] Eggers, Philip E. Irrigation and shroud arrangement for electrically powered endoscopic probes, March 5 1996. US Patent 5,496,314.
[23] Huang, Wen-hu. Free and forced vibration of closely coupled turbomachinery blades. AIAA Journal, 19(7):918– 924, 1981.
[24] Sz, J Kubiak et al. Failure analysis of steam turbine last stage blade tenon and shroud. Engineering Failure Analysis, 14(8):1476–1487, 2007.
[25] Mazur,Zdzislaw,Garcia-Illescas,Rafael,Aguirre-Romano, Jorge, and Perez-Rodriguez, Norberto. Steam turbine blade failure analysis. Engineering Failure Analysis, 15(12):129–141, 2008.
[26] Poursaeidi,E,Aieneravaie,M,andMohammadi,MR. Failureanalysisofasecondstagebladeinagasturbineengine. Engineering failure analysis, 15(8):1111–1129, 2008.
[27] Saito, Akira, Castanier, Matthew P, and Pierre, Christophe. Effectsofacrackedbladeonmistunedturbine engine rotor vibration. Journal of vibration and acoustics, 131(6):061006, 2009.
[28] Lim, Ha Seong, Chung, Jintai, and Yoo, Hong Hee. Modal analysis of a rotating multi-packet blade system. Journal of Sound and Vibration, 325(3):513–531, 2009.
[29] Pennacchi, Paolo, Chatterton, Steven, Bachschmid, Nicolò, Pesatori, Emanuel, and Turozzi, Giorgio. A model to study the reduction of turbine blade vibration using the snubbingmechanism. Mechanical Systems and Signal Processing, 25(4):1260–1275, 2011. ﻧﻮذرﭘﻮر،ﻣﻬﺪیورﻫ،ﻋﺒﺎس.ﺑﺮرﺳﺗﺄﺛﯿﺮﻣﺎنﻣﯿﻠﻪ ﻫﺎیﺣﻠﻘﻮیدرﭘﺮه ﻫﺎی
[٣٠] ﻣﺮﺣﻠﻪآﺧﺮﺗﻮرﺑﯿﻦ ﺑﺨﺎررویﻓﺮﮐﺎﻧﺲ ﻫﺎیﻃﺒﯿﻌآن.ﻓﺼﻠﻨﺎﻣﻪﻣﻬﻨﺪﺳﻣﺎﻧﯿ . ١٣٩١،۴۶ – ٣٧:(٢)۵،ﺟﺎﻣﺪات
[31] Procházka, P and Vaněk, F. Non-contactmethods of sensing vibrations of turbine blades. in 10th International Conf. on Vibrations in Rotating Machinery, pp. 221–231, 2012.
[32] Sanvito, M, Pesatori, E, Bachschmid, N, and Chatterton, S. Analysis of lp steam turbine blade vibrations: experimental results and numerical simulations. in 10th International Conference on Vibrations in Rotating Machinery (VIRM10), pp. 189–197, 2012.
[33] Ma, Hui, Tai, Xingyu, Han, Qingkai, Wu, Zhiyuan, Wang, Di, and Wen, Bangchun. A revised model for rubbing between rotating blade and elastic casing. Journal of Sound and Vibration, 337:301–320, 2015.
[34] Drozdowski, Roman, Völker, Lutz, Häfele, Markus, and Vogt, Damian M. Numerical and experimental analysis of low-pressure steam turbine blades coupled with lacing wire. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 230(3):332– 342, 2016. [35] Afzal, Mohammad, Arteaga, Ines Lopez, and Kari, Leif. An analytical calculation of the jacobian matrix for 3d frictioncontactmodelappliedtoturbinebladeshroudcontact. Computers & Structures, 177:204–217, 2016. رﻫ،ﻋﺒﺎس،ﺳﻤﻮات،ﺑﻬﻨﻮش،وروﺣﺎﻧﺑﺴﻄﺎﻣ،ﻋﺒﺎس.ﺑﺮرﺳآراﯾﺶ ﻫﺎی
[٣۶] ﻣﺨﺘﻠﻒﺑﺮایاﺗﺼﺎلﭘﺮه ﻫﺎیﺗﻮرﺑﯿﻦﺑﺨﺎرﻧﯿﺮوﮔﺎهراﻣﯿﻦاﻫﻮازﺑﻪﻣﻨﻈﻮرﮐﺎﻫﺶ . ٢٠١٧،١۴٢ – ١٣٧:(۴)۴۶،
ارﺗﻌﺎﺷﺎت.ﻣﻬﻨﺪﺳﻣﺎﻧﯿداﻧﺸﺎهﺗﺒﺮﯾﺰ [37]
Xie, Fangtao, Ma, Hui, Cui, Can, and Wen, Bangchun. Vibration response comparison of twisted shrouded blades using different impact models. Journal of Sound and Vibration, 397:171–191, 2017. اﻣﯿﻨ،ﺣﺴﻦ،داداﺷ،اﻣﯿﻦ،وﺑﯿﺎت،ﻧﺎﺻﺮ.ﺑﺮرﺳﺗﺄﺛﯿﺮﺳﯿﻢﻣﺴﺘﻬﻠﮐﻨﻨﺪهﺑﺮ
[٣٨] ﺗﻮرﺑﯿﻦﺑﺨﺎر.دراوﻟﯿﻦﻣﺴﺎﺑﻘﻪﮐﻨﻔﺮاﻧﺲﺑﯿﻦ اﻟﻤﻠﻠ ١۵ارﺗﻌﺎﺷﺎتﭘﺮه ﻫﺎیردﯾﻒ ﺟﺎﻣﻊﻋﻠﻮمﻣﻬﻨﺪﺳدراﯾﺮان.دﺑﯿﺮﺧﺎﻧﻪﮐﻨﻔﺮاﻧﺲ،۵٩٣١ . [39]
Li, Daochun, Wu, Yining, Da Ronch, Andrea, and Xiang, Jinwu. Energy harvesting by means of flow-induced vibrationsonaerospacevehicles.ProgressinAerospaceSciences, 86:28–62, 2016