Follow
abolghassem mesgarpoor Tousi
abolghassem mesgarpoor Tousi
Verified email at aut.ac.ir - Homepage
Title
Cited by
Cited by
Year
Parametric study of injection angle effects on stability enhancement of transonic axial compressors
H Khaleghi, JA Teixeira, AM Tousi, M Boroomand
Journal of propulsion and power 24 (5), 1100-1107, 2008
712008
Role of tip injection in desensitizing the compressor to the tip clearance size
H Khaleghi, MAS Dehkordi, AM Tousi
Aerospace Science and Technology 52, 10-17, 2016
382016
Comparison of turbulence methods in CFD analysis of compressible flows in radial turbomachines
R Aghaei Tog, AM Tousi, A Tourani
Aircraft Engineering and Aerospace Technology 80 (6), 657-665, 2008
372008
A numerical study of the effects of injection velocity on stability improvement in high-speed compressors
H Khaleghi, M Boroomand, JA Teixeira, AM Tousi
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2008
362008
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
Design and CFD analysis of centrifugal compressor for a microgasturbine
R Aghaei tog, A Mesgharpoor Tousi, M Soltani
Aircraft Engineering and Aerospace Technology 79 (2), 137-143, 2007
282007
Stall inception in a transonic axial fan
H Khaleghi, M Boroomand, AM Tousi, JA Teixeira
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2008
272008
Performance adaptation of a 100 kW microturbine
M Kiaee, AM Tousi, M Toudefallah
Applied Thermal Engineering 87, 234-250, 2015
262015
Recirculation casing treatment by using a vaned passage for a transonic axial-flow compressor
H Khaleghi, AM Tousi, M Boroomand, JA Teixeira
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2007
262007
A new approach to off-design performance analysis of gas turbine engines and its application
SM Hosseinimaab, AM Tousi
Energy Conversion and Management 243, 114411, 2021
242021
The effects of compressor blade roughness on the steady state performance of micro-turbines
SS Talebi, AM Tousi
Applied Thermal Engineering 115, 517-527, 2017
242017
Vector-based deterioration index for gas turbine gas-path prognostics modeling framework
M Kiaee, AM Tousi
Energy 216, 119198, 2021
192021
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
R Aghaei-Togh, AM Tousi
Journal of Mechanical Science and Technology 32, 455-464, 2018
112018
A developed methodology in design of highly loaded tandem axial flow compressor stage
H Eshraghi, M Boroomand, AM Tousi
Journal of Applied Fluid Mechanics 9 (1), 83-94, 2015
112015
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
Optimizing the performance of a single-shaft micro gas turbine engine by modifying its centrifugal compressor design
SM Hosseinimaab, AM Tousi
Energy Conversion and Management 271, 116245, 2022
102022
Micro Gas Turbine fault detection and isolation with a combination of Artificial Neural Network and off-design performance analysis
SS Talebi, A Madadi, AM Tousi, M Kiaee
Engineering Applications of Artificial Intelligence 113, 104900, 2022
102022
Experimental investigation of inlet distortion effect on performance of a micro gas turbine
A Naseri, S Sammak, M Boroomand, A Alihosseini, AM Tousi
Journal of Engineering for Gas Turbines and Power 140 (9), 092604, 2018
102018
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
The system can't perform the operation now. Try again later.
Articles 1–20