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    Control oriented modeling of a radial turbine for a turbocharged gasoline engine

    , Article Proceedings of the American Control Conference ; Article number 6580648 , 2013 , Pages 5207-5212 ; ISSN: 07431619 ; ISBN: 9781479901777 Salehi, R ; Shahbakhti, M ; Alasty, A ; Vossoughi, G. R ; Sharif University of Technology
    Abstract
    This paper presents a control oriented model for predicting turbine major variables in a turbocharged spark ignition engine. The turbine is simulated as a two-nozzle chamber where the pressure ratio over the two nozzles is not the same. A convex nonlinear estimation algorithm is formulated to determine the relation between these pressure ratios. The new model is experimentally validated with transient and steady state data collected from a 1.7 liter gasoline engine. The results show the new model can predict the turbine mass flow with an average error of 1.4%. In addition, the application of the turbine model is illustrated for the design of a nonlinear observer to estimate the turbocharger... 

    Aerodynamics Design of Aviation High-speed Radial Turbine with a Feasibility on Cooling

    , M.Sc. Thesis Sharif University of Technology Zolfaghari Nasab Hajizadeh, Abolfazl (Author) ; Ghorbanian, Kaveh (Supervisor)
    Abstract
    Radial turbines with small dimensions and in small power capacities are of great interest. In general, turbine performance improvement and higher output power may be achieved through increasing the inlet mass flow rates however at the expense of more weight and larger dimensions. On the other hand, increasing the inlet total temperature to the turbine will result in higher power potentials. Nevertheless, the turbine needs to be cooled in case that the intended inlet temperature goes beyond the turbine material limitation. In this thesis, radial turbine equations are reviewed and the logic of a 1D algorithm is developed where parameters like the total temperature, total pressure, and mass... 

    Numerical and experimental investigation of the flow and performance characteristics of twin-entry radial turbine under full and partial admission conditions

    , Article 2008 ASME Turbo Expo, Berlin, 9 June 2008 through 13 June 2008 ; Volume 6, Issue PART B , June , 2008 ; 9780791843161 (ISBN) Shahhosseini, M. R ; Hajilouy Benisi, A ; Rad, M ; International Gas Turbine Institute ; Sharif University of Technology
    2008
    Abstract
    In this paper, numerical and experimental investigation of the performance and internal flow field characteristics of the twinentry radial inflow turbine under full and partial admission conditions are presented. The turbine is tested on a turbocharger test facility, which was developed for small and medium size turbochargers. The flow pattern in the volute and impeller of a twin-entry turbine is analyzed using fully three-dimensional viscous program. The computational performance results are compared with the experimental results, and good agreement is found. The flow field at the outlet of the turbine is investigated using a five-hole pressure probe. The tests are performed for both full... 

    Flow and performance characteristics of twin-entry radial turbine under full and extreme partial admission conditions

    , Article Archive of Applied Mechanics ; Volume 79, Issue 12 , 2009 , Pages 1127-1143 ; 09391533 (ISSN) Hajilouy Benisi, A ; Rad, M ; Shahhosseini, M. R ; Sharif University of Technology
    Abstract
    This paper presents numerical and experimental investigation of the performance and internal flow field characteristics of twin-entry radial inflow turbines at full and extreme partial admission conditions. The turbine is tested on a turbocharger test facility, which was developed for small and medium size turbochargers. Experimental results show that the lowest efficiency corresponds to extreme conditions. Therefore, flow field analyzing is employed to consider these conditions. The flow pattern in the volute and impeller of a twin-entry turbine is analyzed using an in-house fully three-dimensional viscous flow solver. The computational performance results are compared with the experimental... 

    A numerical and experimental investigation of the effects of flow ratio on the flow and performance characteristics of a twin entry radial turbine

    , Article Proceedings of the ASME Turbo Expo, 6 June 2011 through 10 June 2011 ; Volume 7, Issue PARTS A, B, AND C , 2011 , Pages 2139-2153 ; 9780791854679 (ISBN) Shahhosseini, M. R ; Hajilouy Benisi, A ; Rajabian, M ; Sharif University of Technology
    Abstract
    In this paper, a numerical and experimental investigation of the performance and internal flow field characteristics of the twin-entry radial inflow turbine under full and partial admission conditions are presented. The turbine is tested on a turbocharger test facility which was developed for small and medium size turbochargers. The flow pattern in the volute and impeller of a twin-entry turbine is analyzed using a fully three-dimensional viscous program. The computational performance results are compared with the experimental results, and good agreement is found. The flow field at the outlet of the turbine is investigated using a five-hole pressure probe. Numerical and experimental results... 

    A new analytical model of a radial turbine and validation by experiments

    , Article IEEE Aerospace Conference Proceedings, 6 March 2010 through 13 March 2010 ; March , 2010 ; 1095323X (ISSN) ; 9781424438884 (ISBN) Pourfarzaneh, H ; Hajilouy Benisi, A ; Farshchi, M ; Sharif University of Technology
    2010
    Abstract
    In the conceptual design phase of a turbocharger, where emphasis is mainly on parametric studies, before manufacturing and tests, a generalized and robust model that applies over a wide range properly, is unavoidable. 12The critical inputs such as turbine maps are not available during the conceptual design phase. Hence, generalized turbine models use alternate methods that work without any supplementary tests and can operate over wide ranges. One of the common and applicable modeling methods in design process is 'Dimensionless Modeling' using the constant coefficient scaling (CCS). This method can almost predict the turbine characteristics at the design point. However, at off-design... 

    Modeling of twin-entry radial turbine performance characteristics based on experimental investigation under full and partial admission conditions

    , Article Scientia Iranica ; Volume 16, Issue 4 B , 2009 , Pages 281-290 ; 10263098 (ISSN) Hajilouy, A ; Rad, M ; Shahhosseini, M. R ; Sharif University of Technology
    2009
    Abstract
    In this paper, the performance of a turbocharger twin-entry radial inflow turbine is investigated analytically and experimentally under steady state, full and partial admission conditions. In this modeling, the mass flow rate, pressure ratio and efficiency of the turbine are assumed unknown. The turbine geometry and the inlet total pressure and temperature are known, hence, the turbine performance characteristics can be obtained. In the turbocharger laboratory, performance characteristics of the turbine are determined, measuring the main parameters for various operating conditions. Comparing the model and experimental results shows good agreement. Also, considering the effect of test...