fa en fa ar fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa ur fa fa fa fa fa fa fa en fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa fa ur fa fa en fa en es de en azb en fa en fr en en en ar en en en en en en en en en en en en en en en en en en en en en fr en en en en en en en fa mzn fa fa el fa fa fa it id en en id bo en en fa ar fa de id fa de bo fa de en fa de en fa fa fa fa fa fa fa fa fa fa ar fa fa fa fa fa fa fa de
مدل‌های آشفتگی معادلات میانگیری رینولدز
عملکرد دور از نقطة طراحی
Prediction of flow separation in a low-pressure turbine cascade at design and off-design operating conditions
[1] Hodson, H. P., R. J. Howell. "Bladerow interactions, transition, andhigh-lift aerofoils in low-pressure turbines." Annual Review of Fluid Mechanics.37, 2005, pp. 71–98.
[2] Hodson, H. P., R. G. Dominy. "The off-design performance of alow-pressure turbine cascade." ASME Journal of Turbomachinery, 109(2), 1987, pp. 201–209.
[3] Stieger, R., H. P. Hodson. "The transition mechanism of highly loadedlow-pressure turbine blades." ASME Journal of Turbomachinery, 126 (4), 2004, pp. 536–543.
[4] Stieger, R., H. P. Hodson. "The unsteady development of a turbulentwake through a downstream low-pressure turbine blade passage." ASME Journal of Turbomachinery, 127 (2), 2005, pp. 388–394.
[5] Opoka, M. M., R. L. Thomas, H. P. Hodson. "Boundary layertransition on the high lift T106A low-pressure turbine blade with an oscillating downstream pressure field." ASME Journal of Turbomachinery, 130(2), 2008.
[6] Coul, J. D., H. P. Hodson. "Unsteady boundary-layer transition in low-pressure turbines." Journal of Fluid Mechanics. 681, 2011, pp. 370-410.
[7] Zhou, C., H. P., Hodson, C. Himmel. "The effects of trailing edge thickness on the losses of ultrahigh lift low pressure turbine blades." ASME Journal of Turbomachinery, 136, 2014, 081011-1–9.
[8] Wu, X. P. A. Durbin. "Evidence of longitudinal vortices evolvedfrom distorted wakes in a turbine passage." Journal of Fluid Mechanics, 446, 2001, pp. 199–228.
[9] Michelassi, V., J. G. Wissink, J. Fröhlich, W. Rodi. "Large-eddysimulation of flow around low-pressure turbine blade with incoming wakes." AIAA Journal, 41 (11), 2003, pp. 2143–2156.
[10] Lodefier, K., E. Dick. "Modelling of unsteady transition inlow-pressure turbine blade flows with two dynamic intermittencyequations." Journal of Flow, Turbulence and Combustion, 76 (2), 2005, pp. 103–132.
[11] Wissink, J. G., W. Rodi, H. P. Hodson. "The influence of disturbancescarried by periodically incoming wakes on the separating flow arounda turbine blade." Journal of Heat and Fluid Flow. 27 (4), pp. 721–729.
[12] Matsuura, K., C. Kato. "Large-eddy simulation of compressibletransitional flows in a low-pressure turbine cascade." AIAA Journal.45 (2), 2007, pp. 442–457.
[13] Velez, C., P. Coronado, H. Al-Kuran, M. Ilie. "Numericalcomputations of turbine blade aerodynamics; comparison of LES, SAS, SST, SA, and k-e. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibi, 2011.
[14] Ghidoni, A., A. Colombo, S. Rebay, F. Bassi. "Simulation of thetransitional flow in a low pressure gas turbine cascade with a high-order discontinuous galerkin method." ASME Journal of Fluids Engineering, 135 (7), 2013, pp. 071 101–8.
[15] Pacciani, R., M., Marconcini, A., Arnone, F. Bertini. "Predicting high-lift low-pressure turbine cascades flow using transition-sensitive turbulence closures." ASME Journal of Turbomachinery, 136: 2014, pp. 1–11.
[16] Zhang, W., Z., Zou, L., Qi, J., Ye, L. Wang. "Effects of freestream turbulence on separated boundary layer in a low-Re high-lift LP turbine blade." Computers and Fluids.109, 2015, pp.1–12.
[17] Nagabhushana Rao, V., P. G., Tucker, R. J., Jeferson-Loveday, J. D., Coull. "Large eddy simulations in low-pressure turbines: Effect of wakes at elevated free-stream turbulence." Int. Journal of Heat and Fluid Flow, 43, 2013, pp. 85–95.
[18] Fottner.L. "Test cases for computation of internal flows in aero enginecomponents." AGARD-AR-275, 1990, pp.112–123.
[19] Hildebrandt, T., L. Fottner. "A numerical study of the influenceof grid refinement and turbulence modeling on the flow field insidea highly loaded turbine cascade." ASME Journal of Turbomachinery. 121 (4), 1999, pp. 709–716.
[20] T106 LP Turbine Database, http://www-g.eng.cam.ac.uk/whittle/T106/Start.html (accessed November 01, 2015)
[21] OpenFOAM, The Open Source CFD Toolbox, User Guide, OpenCFD Ltd., 12 2014.Available online at http://www.openfoam.org (accessed November 02, 2015)
[22] Favre, A. "Equation des Gaz Turbulents Compressibles." Journal de Mecanique, 4(3), 1956, pp. 361-390.
[23] Wilcox, David C. Turbulence Modeling for CFD, 3rd ed. DCW Industries, Inc., 2006.
[24] Launder, B. E., D. B. Spalding. "The numerical computation ofturbulent flows." Journal of Computer Methods in Applied Mechanics and Engineering Articles. 3 (2), 1974, pp. 269–289.
[25] Martin, M. Pino, Ugo Piomelli, and Graham V. Candler. "Subgrid-scale models for compressible large-eddy simulations." Theoretical and Computational Fluid Dynamics 13 (5), 2000, pp. 361-376.
[26] Spalart, P. R., S. R. Allmaras. "A one equation turbulence model foraerodynamic flows." La Recherche Aerospatiale.1, 1994, pp. 5–21.
[27] Stieger, R. D., D. Hollis, H. P. Hodson. "Unsteady surface pressuresdue to wake-induced transition in a laminar separation bubble ona low-pressure cascade." ASME Journal of Turbomachinery, 126 (4), 2004, pp. 544–550.
[28] Calzada, P. D. L., A. Alonso. "Numerical investigation of heat transferin turbine cascades with separated flows." ASME Journal of Turbomachinery, 125 (2), 2003, pp. 260–266.
[29] A. Raab, Duden, I., L. Fottner. "Controlling the secondary flow in a turbine cascade by three-dimensional airfoil design and endwallcontouring." ASME Journal of Turbomachinery, 121, 1999, pp. 191–199.
دوره 4، شماره 1 - شماره پیاپی 1
اصل مقاله 1.76 MB
ارجاع به این مقاله
تعداد مشاهده مقاله: 1,439
تعداد دریافت فایل اصل مقاله: 972
وکیلی‌پور, شیدوش, حبیب‌نیا رمی, مهدی, ریاضی, روزبه, & محمدی, مسعود. (1394). پیش‌بینی جدایش جریان در مجرای توربینی فشارپایین در شرایط طراحی و دور از نقطة طراحی. دانش و فناوری هوافضا, 4(1), 57-69.
شیدوش وکیلی‌پور; مهدی حبیب‌نیا رمی; روزبه ریاضی; مسعود محمدی. "پیش‌بینی جدایش جریان در مجرای توربینی فشارپایین در شرایط طراحی و دور از نقطة طراحی". دانش و فناوری هوافضا, 4, 1, 1394, 57-69.
وکیلی‌پور, شیدوش, حبیب‌نیا رمی, مهدی, ریاضی, روزبه, محمدی, مسعود. (1394). 'پیش‌بینی جدایش جریان در مجرای توربینی فشارپایین در شرایط طراحی و دور از نقطة طراحی', دانش و فناوری هوافضا, 4(1), pp. 57-69.
وکیلی‌پور, شیدوش, حبیب‌نیا رمی, مهدی, ریاضی, روزبه, محمدی, مسعود. پیش‌بینی جدایش جریان در مجرای توربینی فشارپایین در شرایط طراحی و دور از نقطة طراحی. دانش و فناوری هوافضا, 1394; 4(1): 57-69.