Дисертації з теми "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.
Повний текст джерела
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.
Повний текст джерелаCheng, Liangta. "Combined PIV/PLIF measurements in a high-swirl fuel injector flowfield." Thesis, Loughborough University, 2013. https://dspace.lboro.ac.uk/2134/11936.
Повний текст джерелаAhmad, N. T. "Swirl stabilised gas turbine combustion." Thesis, University of Leeds, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356423.
Повний текст джерелаChen, Rui. "Fluidic devices as fuel injectors for natural gas engines." Thesis, Loughborough University, 1997. https://dspace.lboro.ac.uk/2134/13566.
Повний текст джерелаMehdi, Ahad. "Effect of swirl distortion on gas turbine operability." Thesis, Cranfield University, 2014. http://dspace.lib.cranfield.ac.uk/handle/1826/12129.
Повний текст джерелаMoffat, Dominic Luke. "Modelling of atomization and vaporization in industrial gas turbine injectors." Thesis, University of Leeds, 2016. http://etheses.whiterose.ac.uk/13579/.
Повний текст джерелаAbdulsada, Mohammed. "Flashback and blowoff characteristics of gas turbine swirl combustor." Thesis, Cardiff University, 2011. http://orca.cf.ac.uk/24193/.
Повний текст джерелаRunyon, Jon. "Gas turbine fuel flexibility : pressurized swirl flame stability, thermoacoustics, and emissions." Thesis, Cardiff University, 2017. http://orca.cf.ac.uk/100686/.
Повний текст джерелаSharma, 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.
Повний текст джерелаRees, 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.
Повний текст джерелаAbdullah, 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.
Повний текст джерелаKakade, 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.
Повний текст джерелаTokekar, 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.
Повний текст джерелаTitle 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.
Повний текст джерелаTOKEKAR, 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.
Повний текст джерелаBiegger, 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.
Повний текст джерелаLI, 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.
Повний текст джерелаPeriagaram, 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.
Повний текст джерелаSchlüter, 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.
Повний текст джерелаBiegger, Christoph [Verfasser], and 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.
Повний текст джерелаPark, 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.
Повний текст джерелаPh. 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.
Повний текст джерелаDulac, 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.
Повний текст джерелаTurek, 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.
Повний текст джерелаPh.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.
Повний текст джерелаPh. 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.
Повний текст джерелаAbdeh, 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.
Повний текст джерелаWang, 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.
Повний текст джерелаRajamanickam, Kuppuraj. "Studies on Flow Dynamics and Spray Swirl Interactions in Gas Turbine Combustor." Thesis, 2019. https://etd.iisc.ac.in/handle/2005/4936.
Повний текст джерелаKumar, 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.
Повний текст джерелаCaux-Brisebois, Vincent. "Thermo-acoustic Velocity Coupling in a Swirl-stabilized Gas Turbine Model Combustor." Thesis, 2013. http://hdl.handle.net/1807/42704.
Повний текст джерелаGopakumar, R. "Dynamics of Actuated and Interacting Swirl Premixed Flames in Model Gas Turbine Combustors." Thesis, 2020. https://etd.iisc.ac.in/handle/2005/4598.
Повний текст джерелаTaso, Jhy-Ming, and 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.
Повний текст джерелаHuang, 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.
Повний текст джерелаKhateeb, 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.
Повний текст джерелаSunil, 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.
Повний текст джерелаSunil, 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.
Повний текст джерела