A new approach to off-design performance analysis of gas turbine engines and its application von Hosseinimaab, S.M., Tousi, A.M.

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Micro Gas Turbine fault detection and isolation with a combination of Artificial Neural Network and off-design performance analysis von Talebi, S.S., Madadi, A., Tousi, A.M., Kiaee, M.

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Vector-based deterioration index for gas turbine gas-path prognostics modeling framework von Kiaee, Mehrdad, Tousi, A.M.

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Performance adaptation of a 100 kW microturbine von Kiaee, Mehrdad, Tousi, A.M., Toudefallah, M.

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Optimizing the performance of a single-shaft micro gas turbine engine by modifying its centrifugal compressor design von Hosseinimaab, S.M., Tousi, A.M.

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Using inlet guide vane to improve load following ability of solid oxide fuel cell and gas turbine hybrid cycle von Boroumand, M., Tousi, A. M.

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A methodology for identifying the most suitable measurements for engine level and component level gas path diagnostics of a micro gas turbine von Talebi, SS, Tousi, AM, Madadi, A, Kiaee, M

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The effects of compressor blade roughness on the steady state performance of micro-turbines von Talebi, S.S., Tousi, A.M.

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A Developed Methodology in Design of Highly Loaded Tandem Axial Flow Compressor Stage von Eshraghi, H, Boroomand, M, Tousi, A M

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Parametric Study of Injection Angle Effects on Stability of Transonic Axial Compressors von Khaleghi, H, Teixeira, J A, Tousi, A M, Boroomand, M

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A method for calculating inlet distortion effects on stability of split-flow fans von Khaleghi, H., Doulgeris, G., Boroomand, M., Pilidis, P., Tousi, A. M.

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Parametric Study of Injection Angle Effects on Stability Enhancement of Transonic Axial Compressors von Khaleghi, H, Teixeira, J. A, Tousi, A. M, Boroomand, M

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Optimal hybrid fault recovery in a team of unmanned aerial vehicles von Tousi, M.M., Khorasani, K.

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A numerical study of the effects of injection velocity on stability improvement in high-speed compressors von Khaleghi, H, Boroomand, M, Teixeira, J A, Tousi, A M

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Recirculation casing treatment by using a vaned passage for a transonic axial-flow compressor von Khaleghi, H, Tousi, A. M., Boroomand, M, Teixeira, J. A.

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Stall inception in a transonic axial fan von Khaleghi, H, Boroomand, M, Tousi, A M, Teixeira, J A

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Comparison of turbulence methods in CFD analysis of compressible flows in radial turbomachines von Aghaei tog, R., Tousi, A.M., Tourani, A.

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Experimental Investigation of Inlet Distortion Effect on Performance of a Micro Gas Turbine von Naseri, Alireza, Sammak, Shervin, Boroomand, Masoud, Alihosseini, Alireza, Tousi, Abolghasem M

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Multi-objective PFDE algorithm for solving the optimal siting and sizing problem of multiple DG sources von Moradi, Mohammad H., Reza Tousi, S.M., Abedini, Mohammad

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Role of tip injection in desensitizing the compressor to the tip clearance size von Khaleghi, Hossein, Sheikhshahrokh Dehkordi, Mohammad-Amin, Tousi, Abolghasem M.

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