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Total 590 records

    Failure analysis of a first stage gas turbine blade

    , Article Engineering Failure Analysis ; 2010 ; 13506307 (ISSN) Kazempour Liacy, H ; Abouali, S ; Akbari Garakani, M

    Failure analysis of a repaired gas turbine nozzle

    , Article Engineering Failure Analysis ; 13506307 (ISSN) Kazempour Liacy, H ; Abouali, S ; Akbari Garakani, M ; Sharif University of Technology

    Unsteady aerodynamic analysis of different multi-MW horizontal axis wind turbine blade profiles on SST K-ω model

    , Article Green Energy and Technology ; 2018 , Pages 17-30 ; 18653529 (ISSN) Radmanesh, A. R ; Abbaspour, M ; Soltani, M. R ; Sharif University of Technology
    Springer Verlag  2018
    Abstract
    In this study, in order to indicate the best airfoil profile for the different sections of a blade, five airfoils including S8xx, FFA, and AH series were studied. Among the most popular wind power blades for this application were selected, in order to find the optimum performance. Nowadays, modern wind turbines are using blades with multi-airfoils at different sections. On the large scale profile, SST K-ω model with different wind speed at large-scale profile was applied to the simulation of horizontal axis wind turbines (HAWT). The aerodynamic simulation was accomplished using the computational fluid dynamic (CFD) method based on the finite volume method. The governing equations applied in... 

    Load profile flattening considering EV’s initial and final SoC and arrival and departure times

    , Article Iranian Journal of Electrical and Electronic Engineering ; Volume 18, Issue 4 , 2022 ; 17352827 (ISSN) Bagheri, V ; Ehyaei, A. F ; Haeri, M ; Sharif University of Technology
    Iran University of Science and Technology  2022
    Abstract
    In distribution networks, failure to smooth the load curve leads to voltage drop and power quality loss. In this regard, electric vehicle batteries can be used to smooth the load curve. However, to persuade vehicle owners to share their vehicle batteries, we must also consider the owners' profits. A challenging problem is that existing methods do not take into account the vehicle owner demands including initial and final states of charge and arrival and departure times of vehicles. Another problem is that battery capacity of each vehicle varies depending on the type of vehicle; which leads to uncertainties in the charging and discharging dynamics of batteries. In this paper, we propose a... 

    Design of a Small Scale Vertical Axis Wind Turbine

    , M.Sc. Thesis Sharif University of Technology Soltanieh, Hossein (Author) ; Ebrahimi, Abbas (Supervisor) ; Darbandi, Masoud (Supervisor)
    Abstract
    Today, renewable energies such as solar and wind power are replaced to fossil fuel. Wind turbines are two categories; horizontal axis and vertical axis. Vertical axis turbines are not dependent on wind direction and since equipments are installed at the bottom of these turbine towers, maintenance is easy. Among vertical axis turbines, performance of darrieus turbine is better. The aim of this thesis is, analysis and preliminary designing of 1-kilowatt darrieus wind turbine, based on climate of the country, for using in urban environments or areas where there is no economic justification for development of power grid systems. In this regard, statistical data base is made up of vertical axis... 

    Aerodynamic Design and Parametric Investigation of Power Turbine for a Turbo Jet Engine

    , M.Sc. Thesis Sharif University of Technology Mani, Alireza (Author) ; Hajilouy Benisi, Ali (Supervisor)
    Abstract
    In this research, it is aimed to convert a turbojet engine to a turboshaft by replacing the exhaust nozzle with a new designed power turbine stage. The design procedure is backed up with parametric studies to increase efficiency. At first a program is written for one dimensional modelling of the stage of axial turbine. By the way, the three dimensional modelling of the stage of axial turbine with Ansys-cfx business software is done. These methods are validated by modelling the gas generator turbine and comparison of their results with experimental results. Then the power turbine including the blades and the geometry of flow walls on shaft and casing are designed. The performance of power... 

    Developing an improved 1-D thermoflow approach to analyze turbine vane temperature distribution

    , Article AIAA Scitech Forum, 6 January 2020 through 10 January 2020 ; Volume 1 Part F , 6-10 January , 2020 Jalali, R ; Darbandi, M ; Schneider, G. E ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc, AIAA  2020
    Abstract
    This study presents an improved one-dimensional approach, which is coupled with the 3D numerical flow solver, to find the temperature distribution over a typical turbine vane. The developed code solves the one-dimensional flow and heat transfer distribution in cooling flow passages inside a turbine vane. It uses our previous developed version and uses experimental correlations to predict the heat transfer coefficient and friction factor for each cooling passage. On the other hand, the hot gas flow field and conduction inside the vane material are solved using a 3D numerical solver. Our survey shows that cooling channel’s wall temperature has effect on the convective heat transfer coefficient... 

    Experimental modeling of twin-entry radial turbine

    , Article Iranian Journal of Science and Technology, Transaction B: Engineering ; Volume 32, Issue 6 , December , 2008 , Pages 571-584 ; 10286284 (ISSN) Aghaali, H ; Hajilouy Benisi, A ; Sharif University of Technology
    2008
    Abstract
    In this paper the performance characteristics of a turbocharger twin-entry radial inflow gas turbine with asymmetrical volute and rotor tip diameter of 73.6 mm in steady state and under full and partial admission conditions are investigated. The employed method is based on one dimensional performance prediction which is developed for partial admission conditions. Furthermore, this method is developed for the asymmetrical volute of the turbine considering the flow specifications. Experimental investigation of the research was carried out on special test facilities under full and partial admission conditions for a wide range of speeds. A comparison of experimental and modeling results shows... 

    Prediction of transition point on an oscillating airfoil using Neural network

    , Article 2007 5th Joint ASME/JSME Fluids Engineering Summer Conference, FEDSM 2007, San Diego, CA, 30 July 2007 through 2 August 2007 ; Volume 2 FORA, Issue PART A , July , 2007 , Pages 33-39 ; 0791842886 (ISBN); 9780791842881 (ISBN) Soltani, M. R ; Seddighi, M ; Masdari, M ; Sharif University of Technology
    2007
    Abstract
    Dynamic Neural network was used to minimize the amount of data required to predict the location of transition point on a 2-D oscillatory wing. For this purpose, various experimental tests were carried out on a section of a 660kw wind turbine blade. A multi layer non linear perceptrons network was trained using the output signals of four hot films attached on the upper surface of the model. Results show that using only 50% of the test data, the trained network was able to the transition point with an acceptable accuracy. Moreover, the method can predict the transition points at any position of the wing surface for different Reynolds numbers, amplitudes and initial angles of oscillation, and... 

    Effect of surface contamination on the performance of a section of a wind turbine blade

    , Article 45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, 8 January 2007 through 11 January 2007 ; Volume 19 , 2007 , Pages 13026-13036 ; 1563478900 (ISBN); 9781563478901 (ISBN) Soltani, M. R ; Birjandi, A. H ; Sharif University of Technology
    2007
    Abstract
    A series of low speed wind tunnel tests on a section of a 660 Kw wind turbine blade which is under constructer were conducted to examine the effects of distributed surface contamination on its performance characteristics. At first model was tested in the clean condition and after that it was tested with tree different types of roughness. The data shows that this particular airfoil is very sensitive to the applied surface roughness. For the contaminated model the roughness, 0.5mm height was distributed over the entire upper surface of the airfoil such that the distribution pattern was denser in the vicinity of the leading edge and thinner in the trailing edge area. Statistical data show that... 

    Effects of reduced frequency on the performance of a wind turbine blade in the low and high turbulent unsteady flow

    , Article 25th AIAA Applied Aerodynamics Conference, 2007, Miami, FL, 25 June 2007 through 28 June 2007 ; Volume 2 , 2007 , Pages 877-882 ; 10485953 (ISSN); 1563478986 (ISBN); 9781563478987 (ISBN) Soltani, M. R ; Amiralaei, M. R ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2007
    Abstract
    An extensive experimental study is conducted to investigate the effects of reduced frequency on a harmonically pitching wing where its cross section is used in a 660 kW wind turbine under construction in Iran. The corresponding lift coefficient and real time pressure signatures at three sections of the model at various reduced frequencies are examined. The test covers a wide range of angles of attack at prestall, stall, and deep stall regions. Pressure distributions at tip, middle, and root sections of the wing were recorded and from these distributions the lift coefficients are computed. The results show great role of the reduced frequency in altering the maximum lift coefficients, lift... 

    Thermodynamic and environmental consideration of advanced gas turbine cycles with reheat and recuperator

    , Article International Journal of Environmental Science and Technology ; Volume 4, Issue 2 , 2007 , Pages 253-262 ; 17351472 (ISSN) Sheikhbeigi, B ; Ghofrani, M. B ; Sharif University of Technology
    CEERS  2007
    Abstract
    The role of gas turbine power plants in electrical energy production has been considerably increased in the last two to three decades. Various methods have been proposed to improve the performance of gas turbine cycles. In this research, two methods, a reheat cycle and a cycle with a reheat and a recuperator, were investigated and compared with a simple cycle. The main objective of this paper is to study the performance of an simple cycle and reheat cycle under actual conditions. In this regard, all processes are treated as actual, and in particular a relatively simple and reliable approach is used to predict the amount of cooling air. The results obtained on the basis of a model developed... 

    Contamination effects on the performance of a wind turbine blade section

    , Article 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings, San Francisco, CA, 5 June 2006 through 8 June 2006 ; Volume 4 , 2006 , Pages 2801-2805 ; 1563478153 (ISBN); 9781563478154 (ISBN) Soltani, M. R ; Birjandi, A. H ; Sharif University of Technology
    2006
    Abstract
    A series of low speed wind tunnel tests on a section of a 660 Kw wind turbine blade were conducted to examine the effects of distributed surface contamination on its performance. The airfoil was a section of a wind turbine blade under construction. The performance of the section was measured in the following conditions: 1. Clean airfoil 2. Two types of zigzag roughness 3. Strip tape 4. Distributed contamination roughness Our preliminary data shows that the airfoil is very sensitive to the applied surface roughness. For the contamination model the roughness, 0.5mm height, is distributed over the entire upper surface of the airfoil. By putting the contamination roughness on the airfoil the... 

    Experimental investigation of blade number and design effects for a ducted wind turbine

    , Article Renewable Energy ; Volume 105 , 2017 , Pages 334-343 ; 09601481 (ISSN) Ahmadi Asl, H ; Kamali Monfared, R ; Rad, M ; Sharif University of Technology
    Abstract
    Over the recent decades, many different ducted turbines have been designed to augment efficiency of wind turbines. The design and number of blades are the most important parameters to optimize efficiency of wind turbines. In this paper, effects of design, number and attack angles of blades on rotational speed are experimentally studied in a duct which increases wind velocity up to 2.46 times numerically and 2.32 times experimentally as great as far-field flow. In order to realize this, 3 different types of aerodynamic blades were designed and then, 2-bladed, 3-bladed and 4-bladed impellers were created by these blades; finally, 9 impellers were built on aggregate. The rotational speed of... 

    A comparative analysis of the new excitation controlled synchronous generator-based wind turbine

    , Article Scientia Iranica ; Volume 29, Issue 1 D , 2022 , Pages 151-167 ; 10263098 (ISSN) Shamsnia, A ; Parniani, M ; Sharif University of Technology
    Sharif University of Technology  2022
    Abstract
    Excitation Controlled Synchronous Generator-based Wind Turbine (ECSG WT) is a recently proposed Wind Turbine (WT) scheme that has not been fully investigated in detail. This paper intends to analyze the performance of the ECSG WT scheme and compare it with those of two mainstream WT schemes based on electrically excited synchronous generator, i.e., VSC-based full converter WT and diode bridge rectifier-based WT equipped with boost converter on its Direct Current (DC) link. The objective of this comparison is to demonstrate great potentials of ECSG WT to be considered in the wind industry. To do so, two successful Wind Turbine (WT) schemes in the market that are structurally close to ECSG WT... 

    A Pareto optimal multi-objective optimization for a horizontal axis wind turbine blade airfoil sections utilizing exergy analysis and neural networks

    , Article Journal of Wind Engineering and Industrial Aerodynamics ; Volume 136 , January , 2015 , Pages 62-72 ; 01676105 (ISSN) Mortazavi, S. M ; Soltani, M. R ; Motieyan, H ; Sharif University of Technology
    Elsevier  2015
    Abstract
    In this study a multi-objective genetic algorithm is utilized to obtain a Pareto optimal set of solutions for geometrical characteristics of airfoil sections for 10-meter blades of a horizontal axis wind turbine. The performance of the airfoil sections during the process of energy conversion is evaluated deploying a 2D incompressible unsteady CFD solver and the second law analysis. Artificial neural networks are trained employing CFD obtained data sets to represent objective functions in an algorithm which implements exergetic performance and integrity characteristics as optimization objectives. The results show that utilizing the second law approach along with Pareto optimality concept... 

    Turbine blade cooling passages optimization using reduced conjugate heat transfer methodology

    , Article Applied Thermal Engineering ; Volume 103 , 2016 , Pages 1228-1236 ; 13594311 (ISSN) Mazaheri, K ; Zeinalpour, M ; Bokaei, H. R ; Sharif University of Technology
    Elsevier Ltd  2016
    Abstract
    Here we have optimized shape and location of cooling passages of a C3X turbine blade using a multi-objective strategy. The objective functions is selected to be the maximum temperature gradient and the maximum temperature through the three dimensional blade. Shape of cooling channels is modeled using a new method based on the Bezier curves and using forty design variables. The optimized channel shapes are found to be smooth and without corners. To reduce the computational time, parallel processing and the reduced conjugate heat transfer methodology RCHT is used. Using RCHT, the heat transfer between channels and blade are coupled, while the experimental data is used for heat transfer... 

    Starting improvement of micro-wind turbines operating in low wind speed regions

    , Article International Journal of Green Energy ; Volume 14, Issue 11 , 2017 , Pages 868-877 ; 15435075 (ISSN) Amir Nazmi Afshar, P ; Gooya, M ; Hosseini, S. V ; Pourrajabian, A ; Sharif University of Technology
    Abstract
    The study deals with the design and optimization of external and internal geometry of micro-wind turbines blades. A specified objective function which consists of the power coefficient and the starting time was defined and the genetic algorithm optimization technique in conjunction with the blade-element momentum theory was adopted to find the geometry of the blades including the distributions of the chord, the twist angle and also the shell thickness. Moreover, the allowable stress of the blades was considered as a constraint to the objective function. Results show that a reasonable compromise is achievable such that the starting time of the blades reduces noticeably in return for a small... 

    Experimental study on gyroscopic effect of rotating rotor and wind heading angle on floating wind turbine responses

    , Article International Journal of Environmental Science and Technology ; Volume 15, Issue 12 , 2018 , Pages 2531-2544 ; 17351472 (ISSN) Bahramiasl, S ; Abbaspour, M ; Karimirad, M ; Sharif University of Technology
    Abstract
    Limited fossil resources, daily increasing rate of demand for energy and the environmental pollution fact have made people revert to renewable sources of energy as a solution. One type of renewable energy is offshore wind energy which has high potential without any sound and visual noises. Recently, a lot of researchers have carried out on the issue of offshore wind turbine. Because of incapability of most of software programs to simulate gyroscopic effect of rotating rotors, in this articles a significant effort has been made to fabricate and test an offshore wind turbine under different rotor rotation velocities and different heading angle of wind so as to obtain the effects of these... 

    Aeroelastic modeling and dynamic analysis of a wind turbine rotor by considering geometric nonlinearities

    , Article Journal of Sound and Vibration ; Volume 432 , 2018 , Pages 653-679 ; 0022460X (ISSN) Rezaei, M. M ; Zohoor, H ; Haddadpour, H ; Sharif University of Technology
    Academic Press  2018
    Abstract
    Due to the increased flexibility of modern multi-megawatt wind turbine structures, more advanced analyses are needed to investigate the effects of geometric nonlinearities originating from large blade deformations under operational loads. The main objective of this paper is to study the related dynamics and the aeroelastic effects of these nonlinearities by using a multi-flexible-body aeroelastic model of an entire three-bladed wind turbine assembly instead of a more conventional single-blade model. A geometrically-exact beam formulation is employed to model the rotating blades connected to the wind turbine tower tip via hub and nacelle components; and the revolute joint constraint is...