Investigation on the aerodynamic performance and boundary layer characteristics of high deflection industrial turbine cascade at off-design conditions von Ghandi, Hamed, Togh, Reza Aghaei, Tousi, Abolghasem M.

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Effects of nozzle arrangement angle on the performance of partially admitted turbines von Aghaei-Togh, Reza, Tousi, Abolghasem M.

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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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Performance Analysis of Axial Flow Compressor and Part Load Consideration in a Gas Turbine Application von ASLI, Majid, TOUSI, Abolghasem M.

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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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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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The Effect of Variable Stator on Performance of a Highly Loaded Tandem Axial Flow Compressor Stage von Eshraghi, Hamzeh, Boroomand, Masoud, Tousi, Abolghasem M., Fallah, Mohammad Toude, Mohammadi, Ali

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Experimental and numerical investigation of design optimization of a partial admitted supersonic turbine von Aghaei tog, Reza, Tousi, Abolghasem M.

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