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Reza Aghaei Togh
Reza Aghaei Togh
Assistant Professor, Dep. of Aerospace Eng., Science and Research Branch of IAU
Verified email at srbiau.ac.ir - Homepage
Title
Cited by
Cited by
Year
Experimental and numerical investigation of design optimization of a partial admitted supersonic turbine
AM Tousi
Propulsion and Power Research 2 (1), 70-83, 2013
302013
Improving of the micro-turbine’s centrifugal impeller performance by changing the blade angles
RA Tough, AM Tousi, J Ghaffari
ICCES 14 (1), 1-22, 2010
122010
Effects of nozzle arrangement angle on the performance of partially admitted turbines
AT Reza, MT Abolghasem
Journal of Mechanical Science and Technology 32 (1), 455-464, 2018
112018
Flow pattern improvement in nozzle-rotor axial gap in impulse turbine
R Aghaei tog, A Mesgarpoor Tousi
Aircraft Engineering and Aerospace Technology: An International Journal 86 …, 2014
112014
An empirical model for partially admitted turbine efficiency
R Aghaei tog, A Mesgarpoor Tousi
Aircraft Engineering and Aerospace Technology: An International Journal 87 …, 2015
102015
Numerical and experimental evaluation of supersonic turbine flow and effect of geometrical change of blade edges on turbine performance
TOGR AGHAEI, AM Tousi, M Boroomand
JOURNAL OF APPLIED AND COMPUTATIONAL SCIENCES IN MECHANICS (JOURNAL OF …, 2011
92011
Design Optimization of a Partial Admitted Supersonic Turbine Using Genetic Algorithm and 3D Numerical Analysis
R Aghaei Tog, AM Tousi, M Boroomand
ASME International Mechanical Engineering Congress and Exposition 45172, 15-26, 2012
52012
Finding an optimal blade-profile to improving the performance of partially admitted turbines
RA Togh, MM Karimi
Aircraft Engineering and Aerospace Technology 92 (6), 863-877, 2020
32020
Numerical Study of the Effects of Blade Angles on the Performance of Centrifugal Impellers
R Aghaei-Tog, J Ghaffari, A Mesgharpoor-Tousi, M Boroumand
Journal of Aerospace Mechanics 8 (2), 93-100, 2012
22012
Study of three types of wave leading edge on the performance of industrial turbine blade cascade
H Ghandi, R Aghaei Togh, A Mesgarpoor Tousi
Aircraft Engineering and Aerospace Technology 93 (1), 105-114, 2021
12021
Improving the Aerodynamic Performance of Radial Gas Microturbine with Double Curvature Blades
R Aghaei Togh, M Ahmadi, M Nobakhti
Technology in Aerospace Engineering 4 (4), 21-30, 2021
12021
Investigation on the aerodynamic performance and boundary layer characteristics of high deflection industrial turbine cascade at off-design conditions
H Ghandi, RA Togh, AM Tousi
Journal of Mechanical Science and Technology 34, 5261-5269, 2020
12020
Numerical Investigation of the Effects of Minor Geometric Changes of the Stator Blade Profiles on the Steady Performance of a High-pressure Gas-turbine
AH Babaei, R Aghaei Togh, MH Nobakhti, MJ Montazeri
Modares Mechanical Engineering 19 (5), 1209-1220, 2019
12019
Experimental Evaluation of Supersonic Turbine Characteristic Curve at Full and Partial Admission in Turbine Test Rig
R Aghaei Togh, A Mesgarpoor Tousi
Journal of Applied and Computational Sciences in Mechanics 28 (2), 1-20, 2017
12017
Analysis and identification of the flow pattern in a specific high-pressure axial turbine in off-design conditions
S Saharkhiz, R Aghaei Togh
Technology in Aerospace Engineering 8 (3), 47-61, 2024
2024
Investigation of the Difference Between Ordinary and FSI Numerical Solution for Flutter of Tandem Compressor.
AS Benis, R Aghaei-Togh
International Journal of Acoustics & Vibration 28 (4), 2023
2023
Multi-objective multidisciplinary design optimization of liquid-propellant engines thrust chamber based on a surrogate model
HR Alimohammadi, R Aghaei-Togh
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2023
2023
Improving the performance and work-absorbing capacity of the axial-flow compressor by using tandem blades.
A Sekhavat Benis, R Aghaei Togh
Journal of Aerospace Science and Technology 16 (1), 146-158, 2023
2023
بهبود عملکرد و افزایش ظرفیت جذب کار در کمپرسور محوری با به‌کارگیری پره‌های تاندم.
A Sekhavat Banis, R Aghaei Togh
علوم و مهندسی هوافضا, 2022
2022
Three-Dimensional Study of the Effect of Tandem Compressor Pressure Ratio on Downstream Vortices
A Sekhavat Benis, R Aghaei Togh
Fluid Mechanics & Aerodynamics Journal 11 (1), 145-157, 2022
2022
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