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    Numerical Study on Improvement of Performance of Savonius Wind Turbine with Curtaining

    , M.Sc. Thesis Sharif University of Technology Emdad, Amir Hossein (Author) ; Shamloo, Amir (Supervisor) ; Sadrhosseini, Hani (Supervisor)
    Abstract
    In this study, the performance of an existing Savonius turbine has been improved through designing a curved curtain, the curtain has been placed in front of the rotor. To do so, the main purpose is to increase the net static torque of wind rotor via a newly designed curtain. A new guide vane is designed to prevent negative torque produced by convex surface of wind rotor and increasing wind velocity which is impacted concave side of wind turbine rotor blade. The numerical modeling of flow field is verified by experimental result for wind rotor without straightener. The numerical code verification accomplished at three different angle of rotation which the biggest difference between... 

    Exploring the Possibility of Improving the Performance of a Steam Turbine Applying the Data Mining Approach on the Real Data Collected from the Related Power Cycle

    , M.Sc. Thesis Sharif University of Technology Atarodi, Mahmood (Author) ; Darbandi, Masoud (Supervisor)
    Abstract
    The steam turbines share a significant part of Iran's electricity production. Evidently improving the performance of these steam turbines will improve the performance of power plants and enhance the capability of power production in Iran. Since the behavior of steam turbines is highly nonlinear and that it is affected by various factors, it is difficult to determine the optimum operating conditions for each turbine in specific unit of a power plant. In addition, it is very difficult to model the turbine behavior based on the mathematical equations. Fortunately a large amount of information is collected and stored annually by the data-processing systems in each power plant. These collected... 

    Recuperator Design of a 100kW Aviation Gas Turbine and its Integrated Performance Analysis with the Aircraft

    , M.Sc. Thesis Sharif University of Technology Shokati, Moosarreza (Author) ; Ghorbanian, Kaveh (Supervisor)
    Abstract
    The increasing need for more efficient and environmentally friendly microturbines necessitates the utilization of compact recuperators resulting in lower fuel consumption and emissions. The goal of this research is to determine the performance behavior of a primary surface recuperator to be incorporated in a 100 kW microturbine. Primary surface recuperator, known for relatively favorable characteristics in heat transfer, low weight, and high efficiency is considered as a candidate in aviation engines. In this research, a computational model for heat transfer and pressure losses is used for the design optimization of annular involute-profile cross wavy primary surface recuperators in... 

    A new semi-empirical wind turbine capacity factor for maximizing annual electricity and hydrogen production

    , Article International Journal of Hydrogen Energy ; Volume 45, Issue 32 , 2020 , Pages 15888-15903 Sedaghat, A ; Mostafaeipour, A ; Rezaei, M ; Jahangiri, M ; Mehrabi, A ; Sharif University of Technology
    Elsevier Ltd  2020
    Abstract
    The capacity factor is an important wind turbine parameter which is ratio of average output electrical power to rated electrical power of the wind turbine. Another main factor, the AEP, the annual energy production, can be determined using wind characteristics and wind turbine performance. Lower rated power may lead to higher capacity factor but will reduce the AEP. Therefore, it is important to consider simultaneously both the capacity factor and the AEP in design or selecting a wind turbine. In this work, a new semi-empirical secondary capacity factor is introduced for determining a rated wind speed at which yearly energy and hydrogen production obtain a maximum value. This capacity factor... 

    Multi-point optimization of lean and sweep angles for stator and rotor blades of an axial turbine

    , Article Proceedings of the ASME Turbo Expo ; Vol. 2C, issue , 2014 Asgarshamsi, A ; Hajilouy-Benisi, A ; Assempour, A ; Pourfarzaneh, H
    Abstract
    In this research, numerical optimization of the rear part of a gas turbine, consisting of a single stage axial turbine is carried out. Automated aerodynamic shape optimization is performed by coupling a CFD flow simulation code with the Genetic Algorithm. An effective multi-point optimization method to improve efficiency and/or pressure ratio of the axial turbine is performed. Some variations of optimization parameters such as lean and sweep angels of stator and rotor blades are accomplished. Furthermore, during the optimization process, three-dimensional and turbulent flow field is numerically investigated using a compressible Navier-Stokes solver. The gas turbine experimental... 

    Optimum design and sensitivity analysis of axial flow compressor with combination of analytical method, qualitative and quantitative rules and genetic algorithm

    , Article Proceedings of the ASME Turbo Expo, 9 June 2008 through 13 June 2008, Berlin ; Volume 6, Issue PART C , 2008 , Pages 2501-2508 ; 9780791843161 (ISBN) Soltani, M. R ; Khaledi, H ; Ghofrani, M. B ; Rezaei, A. A ; International Gas Turbine Institute ; Sharif University of Technology
    2008
    Abstract
    Simulation and prediction of gas turbine performance is a very important issue in design process or in actual behavior analysis. In these models physical behavior of components such as compressors, combustion chambers and turbines are simulated related to each other. The compressor is the most important part of simulation. This paper presents a model for simulating a compressor using stage stacking procedure with the aid of a genetic algorithm. The most important feature of the proposed method is that qualitative and quantitative rules based on turbo-machinery knowledge of compressors are used as constraints to the genetic algorithm to find the corrected situations of design. This knowledge... 

    A novel design and performance optimization methodology for hydraulic Cross-Flow turbines using successive numerical simulations

    , Article Renewable Energy ; Volume 169 , 2021 , Pages 1402-1421 ; 09601481 (ISSN) Mehr, G ; Durali, M ; Khakrand, M. H ; Hoghooghi, H ; Sharif University of Technology
    Elsevier Ltd  2021
    Abstract
    This paper introduces a new methodology for designing and optimizing the performance of hydraulic Cross-Flow turbines for a wide range of operating conditions. The methodology is based on a one-step approach for the system-level design phase and a three-step, successive numerical analysis approach for the detail design phase. Compared to current design methodologies, not only does this approach break down the process into well-defined steps and simplify it, but it also has the advantage that once numerical simulations are conducted for a single turbine, most of the results can be used for an entire class of Cross-Flow turbines. In this paper, after a discussion of the research background, we... 

    Nonlinear pitch angle control of an onshore wind turbine by considering the aerodynamic nonlinearities and deriving an aeroelastic model

    , Article Energy Systems ; 2021 ; 18683967 (ISSN) Golnary, F ; Moradi, H ; Tse, K. T ; Sharif University of Technology
    Springer Science and Business Media Deutschland GmbH  2021
    Abstract
    In this paper, the control problem of a wind turbine in region 3 (where the wind velocity is between the rated wind velocity and cut out wind velocity) has been investigated by considering the aerodynamic nonlinear behavior of the wind-structure interaction. The model has been developed by using the blade element momentum (BEM) theory to obtain the aerodynamic torque and aerodynamic loads in edgewise and flapwise directions. For validation, the aerodynamic behavior of the onshore NREL 5 MW turbine has been compared with the Fatigue, Aerodynamics, Structures, and Turbulence (FAST) aeroelastic code in terms of the power coefficient. Wind speed is modelled as a three-dimensional profile with... 

    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...