Tesis sobre el tema "Gas Turbine Swirl Injectors"
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Homitz, Joseph. "A Lean-Premixed Hydrogen Injector with Vane Driven Swirl for Application in Gas Turbines". Thesis, Virginia Tech, 2006. http://hdl.handle.net/10919/36334.
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Numerous efforts have been made to develop gas turbine fuel injectors that premix methane/natural gas and air in fuel lean proportions prior to the reaction zone. Application of this technique to hydrogen combustion has been limited due to hydrogen's high flame rate and the concern of the reaction zone propagating into the premixing injector, commonly referred to as flashback. In this investigation, a lean-premixing hydrogen injector has been developed for application in small gas turbines. The performance of this injector was characterized and predictions about the injector's performance operating under combustor inlet conditions of a PT6-20 Turboprop have been made.
Master of Science
Anning, Grant Hugh Gary. "The Effect of Fuel Injector Geometry on the Flow Structure of a Swirl Stabilized Gas Turbine Burner". University of Cincinnati / OhioLINK, 2002. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1024672199.
Texto completoCheng, Liangta. "Combined PIV/PLIF measurements in a high-swirl fuel injector flowfield". Thesis, Loughborough University, 2013. https://dspace.lboro.ac.uk/2134/11936.
Texto completoAhmad, N. T. "Swirl stabilised gas turbine combustion". Thesis, University of Leeds, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356423.
Texto completoChen, Rui. "Fluidic devices as fuel injectors for natural gas engines". Thesis, Loughborough University, 1997. https://dspace.lboro.ac.uk/2134/13566.
Texto completoMehdi, Ahad. "Effect of swirl distortion on gas turbine operability". Thesis, Cranfield University, 2014. http://dspace.lib.cranfield.ac.uk/handle/1826/12129.
Texto completoMoffat, Dominic Luke. "Modelling of atomization and vaporization in industrial gas turbine injectors". Thesis, University of Leeds, 2016. http://etheses.whiterose.ac.uk/13579/.
Texto completoAbdulsada, Mohammed. "Flashback and blowoff characteristics of gas turbine swirl combustor". Thesis, Cardiff University, 2011. http://orca.cf.ac.uk/24193/.
Texto completoRunyon, Jon. "Gas turbine fuel flexibility : pressurized swirl flame stability, thermoacoustics, and emissions". Thesis, Cardiff University, 2017. http://orca.cf.ac.uk/100686/.
Texto completoSharma, Anshu. "Numerical Investigation of a Swirl Induced Flameless Combustor for Gas Turbine Applications". University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1613731788158991.
Texto completoRees, Simon John. "Hydrodynamic instability of confined jets & wakes & implications for gas turbine fuel injectors". Thesis, University of Cambridge, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.609152.
Texto completoAbdullah, Abu Hasan. "The application of high inlet swirl angles for broad operating range turbocharger compressor". Thesis, University of Bath, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.320555.
Texto completoKakade, Vinod. "Fluid Dynamic and Heat Transfer Measurements in Gas Turbine Pre-Swirl Cooling Systems". Thesis, University of Bath, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.503370.
Texto completoTokekar, Devkinandan Madhukar. "Modeling and simulation of reacting flows in lean-premixed swirl-stabilized gas turbine combustor". Cincinnati, Ohio : University of Cincinnati, 2005. http://www.ohiolink.edu/etd/view.cgi?acc%5Fnum=ucin1141412599.
Texto completoTitle from electronic thesis title page (viewed Apr. 18, 2006). Includes abstract. Keywords: Large Eddy Simulation; LES; Lean Pre-mixed; LPM; Gas Turbine Combustor; Combustion; Reacting Flows. Includes bibliographical references.
Dsouza, Jason Brian. "Numerical Analysis of a Flameless Swirl Stabilized Cavity Combustor for Gas Turbine Engine Applications". University of Cincinnati / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1627663015527799.
Texto completoTOKEKAR, DEVKINANDAN MADHUKAR. "MODELING AND SIMULATION OF REACTING FLOWS IN LEAN-PREMIXED SWIRL-STABLIZED GAS TURBINE COMBUSTOR". University of Cincinnati / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1141412599.
Texto completoBiegger, Christoph [Verfasser]. "Flow and Heat Transfer Investigations in Swirl Tubes for Gas Turbine Blade Cooling / Christoph Biegger". München : Verlag Dr. Hut, 2017. http://d-nb.info/1135595984/34.
Texto completoLI, GUOQIANG. "EMISSIONS, COMBUSTION DYNAMICS, AND CONTROL OF A MULTIPLE SWIRL COMBUSTOR". University of Cincinnati / OhioLINK, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1092767684.
Texto completoPeriagaram, Karthik Balasubramanian. "Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging". Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/45828.
Texto completoSchlüter, Jörg Uwe. "Large Eddy Simulations of flow and mixing in jets and swirl flows : application to a gas turbine". Toulouse, INPT, 2000. http://www.theses.fr/2000INPT015H.
Texto completoBiegger, Christoph [Verfasser] y Bernhard [Akademischer Betreuer] Weigand. "Flow and heat transfer investigations in swirl tubes for gas turbine blade cooling / Christoph Biegger ; Betreuer: Bernhard Weigand". Stuttgart : Universitätsbibliothek der Universität Stuttgart, 2017. http://d-nb.info/1132546524/34.
Texto completoPark, Suhyeon. "Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows". Diss., Virginia Tech, 2018. http://hdl.handle.net/10919/82349.
Texto completoPh. D.
Midgley, Kristofer. "An isothermal experimental study of the unsteady fluid mechanics of gas turbine fuel injector flowfields". Thesis, Loughborough University, 2005. https://dspace.lboro.ac.uk/2134/10755.
Texto completoDulac, Adrien. "A CFD Analysis towards Flow Characteristics of three Pre-swirler Designs". Thesis, KTH, Kraft- och värmeteknologi, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-103890.
Texto completoTurek, Louis James. "CONCENTRATION AND VELOCITY FIELDS THROUGHOUT THE FLOW FIELD OF SWIRLING FLOWS IN GAS TURBINE MIXERS". Doctoral diss., University of Central Florida, 2004. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/4392.
Texto completoPh.D.
Department of Mechanical, Materials and Aerospace Engineering
Engineering and Computer Science
Mechanical, Materials and Aerospace Engineering
Kedukodi, Sandeep. "Numerical Analysis of Flow and Heat Transfer through a Lean Premixed Swirl Stabilized Combustor Nozzle". Diss., Virginia Tech, 2017. http://hdl.handle.net/10919/77393.
Texto completoPh. D.
Cornwell, Michael. "Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines". University of Cincinnati / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323433.
Texto completoAbdeh, Hamed. "Incidence Effects on Aerodynamic and Thermal Performance of a Film-Cooled Gas Turbine Nozzle Guide Vane". Doctoral thesis, Università degli studi di Bergamo, 2018. http://hdl.handle.net/10446/105183.
Texto completoWang, Shanwu. "Vortical flow dynamics and acoustic response of gas-turbine swirl-stabilized injectors". 2002. http://etda.libraries.psu.edu/theses/approved/PSUonlyIndex/ETD-218/index.html.
Texto completoRajamanickam, Kuppuraj. "Studies on Flow Dynamics and Spray Swirl Interactions in Gas Turbine Combustor". Thesis, 2019. https://etd.iisc.ac.in/handle/2005/4936.
Texto completoKumar, Sonu. "Experimental Investigation of Novel High Shear Injector at Elevated Pressure Conditions: Hydrodynamics, Spray and Combustion Characterization". Thesis, 2022. https://etd.iisc.ac.in/handle/2005/5949.
Texto completoCaux-Brisebois, Vincent. "Thermo-acoustic Velocity Coupling in a Swirl-stabilized Gas Turbine Model Combustor". Thesis, 2013. http://hdl.handle.net/1807/42704.
Texto completoGopakumar, R. "Dynamics of Actuated and Interacting Swirl Premixed Flames in Model Gas Turbine Combustors". Thesis, 2020. https://etd.iisc.ac.in/handle/2005/4598.
Texto completoTaso, Jhy-Ming y 曹志明. "Prediction on The Interaction of Swirl Flow and Jet In a Gas Turbine-Combustor". Thesis, 1995. http://ndltd.ncl.edu.tw/handle/58283033385393404423.
Texto completoHuang, Ying. "Modeling and simulation of combustion dynamics in lean-premixed swirl-stabilized gas-turbine engines". 2003. http://etda.libraries.psu.edu/theses/approved/WorldWideIndex/ETD-417/index.html.
Texto completoKhateeb, Abdulrahman A. "Stability Limits and Exhaust Emissions from Ammonia Flames in a Swirl Combustor at Elevated Pressures". Diss., 2020. http://hdl.handle.net/10754/666164.
Texto completoSunil, Sanadi Dilip. "Dynamics of Hollow Cone Spray in an Unconfined, Isothermal, Co-Annular Swirling Jet Environment". Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3866.
Texto completoSunil, Sanadi Dilip. "Dynamics of Hollow Cone Spray in an Unconfined, Isothermal, Co-Annular Swirling Jet Environment". Thesis, 2015. http://etd.iisc.ernet.in/2005/3866.
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