رضا تقوی زنوز

سمتهای علمی و اجرایی در دانشگاهها و مراکز علمی کشور

عضو هیات علمی دانشگاه علم و صنعت ایران

مقالات بین المللی خارج از کشور

"Transitional flow in a two-stage low-pressure axial turbine under different clocking of blades", Elsevier BV, (2024), Vol 151, No : 109254
"Aerodynamic design of a high-efficiency two-stage axial turbine, using streamline curvature method and performance optimisation by clocking of stator blades", Cambridge University Press (CUP), (2024), Vol 128, No 1326: 1814-1843
"Clocking effects on aerodynamics of a gas turbine low pressure axial turbine, part 2: Unsteady simulation", SAGE Publications, (2023), Vol 238, No 1: 135-154
"Investigation of inlet distortion effects on axial compressor performance based on streamline curvature method", Polish Society of Theoretical and Applied Mechanics, (2018), Vol , No : 1005
"Improvement of aerodynamic performance of a low speed axial compressor rotor blade row through air injection", Elsevier BV, (2018), Vol 72, No : 409-417
"Experimental investigation on flow unsteadiness during spike stall suppression process in an axial compressor via air injection", SAGE Publications, (2016), Vol 231, No 14: 2677-2688
"Performance Enhancement of a Low Speed Axial Compressor Utilizing Simultaneous Tip Injection and Casing Treatment of Groove Type", The Korean Society for Aeronautical & Space Sciences, (2017), Vol 18, No 1: 91-98
"Performance Enhancement of Centrifugal Compressors Utilizing Impeller Tip Injection", Oxford University Press (OUP), (2016), Vol 32, No 4: 453-461
"Alleviation of spike stall in axial compressors utilizing grooved casing treatment", Elsevier BV, (2015), Vol 28, No 3: 649-658
"Multiple spike stall cells in low speed axial compressor rotor blade row", Polish Society of Theoretical and Applied Mechanics, (2015), Vol , No : 47
"Centrifugal compressor performance assessment under different impeller tip clearance sizes from far to near stall conditions", EDP Sciences, (2014), Vol 15, No 4: 253-265
"Stall margin improvement of a centrifugal compressor utilizing various stepped tip gap configurations", SAGE Publications, (2014), Vol 228, No 7: 772-781
"Stall Inception and Development Process Due to Tip Leakage Flow in Axial Compressor Rotor Blades Row", Oxford University Press (OUP), (2014), Vol 30, No 3: 307-313
"Experimental Investigation of the Loss Coefficients in a Linear Cascade", Walter de Gruyter GmbH, (2014), Vol 31, No 2:
"Effects of casing treatment on behavior of tip leakage flow in an isolated axial compressor rotor blade row", Informa UK Limited, (2013), Vol 36, No 7: 819-830
"Newly Developed Empirical Correlations for Simulation of Transitional Flows", SAGE Publications, (2013), Vol 5, No :
"Numerical simulation of unsteady tip clearance flow in an isolated axial compressor rotor blades row", SAGE Publications, (2011), Vol 226, No 1: 82-93
"Prediction of laminar, transitional and turbulent flow regimes, based on three-equation <i>k</i>-ω turbulence model", Cambridge University Press (CUP), (2008), Vol 112, No 1134: 469-476
"Preliminary design optimization of profile losses in multi-stage axial compressors based on complex method", SAGE Publications, (2008), Vol 222, No 7: 951-961
"Hot-wire anemometry of transitional boundary layers exposed to different freestream turbulence intensities", SAGE Publications, (2008), Vol 222, No 3: 347-356
"Reynolds number effects on the flow around 2-D ellipses at incidence", American Institute of Aeronautics and Astronautics, (1995), Vol , No :

مقالات کنفرانسهای داخلی

مقالات ژورنالهای تخصصی داخلی

تحصیلات تخصصی

دکتری تخصصی مهندسی مکانیک منچستر انگلستان1372-1376
کارشناسی ارشد مهندسی مکانیک دانشگاه صنعتی شریف1364-1366
کارشناسی دانشکده مهندسی مکانیک دانشگاه علم و صنعت ایران1360-1364

آقای دکتر رضا تقوی زنوز

Dr. Reza Taghavi Zonouz

استاد دانشکده مهندسی مکانیک و هوا و فضا - دانشگاه علم و صنعت ایران