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Статті в журналах з теми "Gas Turbine Swirl Injectors"
McGuirk, J. J. "The aerodynamic challenges of aeroengine gas-turbine combustion systems." Aeronautical Journal 118, no. 1204 (June 2014): 557–99. http://dx.doi.org/10.1017/s0001924000009386.
Повний текст джерелаWoo, Seongphil, Jungho Lee, Yeoungmin Han, and Youngbin Yoon. "Experimental Study of the Combustion Efficiency in Multi-Element Gas-Centered Swirl Coaxial Injectors." Energies 13, no. 22 (November 19, 2020): 6055. http://dx.doi.org/10.3390/en13226055.
Повний текст джерелаSo, Younseok, Yeoungmin Han, and Sejin Kwon. "Combustion Characteristics of Multi-Element Swirl Coaxial Jet Injectors under Varying Momentum Ratios." Energies 14, no. 13 (July 5, 2021): 4064. http://dx.doi.org/10.3390/en14134064.
Повний текст джерелаBaba-Ahmadi, M. H., and G. R. Tabor. "Inlet Conditions for Large Eddy Simulation of Gas-Turbine Swirl Injectors." AIAA Journal 46, no. 7 (July 2008): 1782–90. http://dx.doi.org/10.2514/1.35259.
Повний текст джерелаPham, Vu Thanh Nam. "AN IMAGE PROCESSING APPROACH FOR DETERMINING THE SPRAY CONE ANGLE OF A PRESSURE SWIRL INJECTOR EQUIPPED IN A GAS-TURBINE ENGINE." Journal of Science and Technique 16, no. 2 (August 29, 2022): 33–47. http://dx.doi.org/10.56651/lqdtu.jst.v16.n02.265.
Повний текст джерелаJohnson, M. R., D. Littlejohn, W. A. Nazeer, K. O. Smith, and R. K. Cheng. "A comparison of the flowfields and emissions of high-swirl injectors and low-swirl injectors for lean premixed gas turbines." Proceedings of the Combustion Institute 30, no. 2 (January 2005): 2867–74. http://dx.doi.org/10.1016/j.proci.2004.07.040.
Повний текст джерелаWANG, SHANWU, VIGOR YANG, GEORGE HSIAO, SHIH-YANG HSIEH, and HUKAM C. MONGIA. "Large-eddy simulations of gas-turbine swirl injector flow dynamics." Journal of Fluid Mechanics 583 (July 4, 2007): 99–122. http://dx.doi.org/10.1017/s0022112007006155.
Повний текст джерелаVandervort, C. L. "9 ppm NOx/CO Combustion System for “F” Class Industrial Gas Turbines." Journal of Engineering for Gas Turbines and Power 123, no. 2 (January 1, 2001): 317–21. http://dx.doi.org/10.1115/1.1362661.
Повний текст джерелаLezsovits, Ferenc, Sándor Könczöl, and Krisztián Sztankó. "CO emission reduction of a HRSG duct burner." Thermal Science 14, no. 3 (2010): 845–54. http://dx.doi.org/10.2298/tsci1003845l.
Повний текст джерелаCorrea, S. M., A. J. Dean, and I. Z. Hu. "Combustion Technology for Low-Emissions Gas-Turbines:Selected Phenomena Beyond NOx." Journal of Energy Resources Technology 118, no. 3 (September 1, 1996): 193–200. http://dx.doi.org/10.1115/1.2793862.
Повний текст джерелаДисертації з теми "Gas Turbine Swirl Injectors"
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 джерелаКниги з теми "Gas Turbine Swirl Injectors"
B, Kennedy J., Russell S, and United States. National Aeronautics and Space Administration., eds. Fuel-injector/air-swirl characterization. [Washington, DC: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаB, Kennedy J., Russell S, and United States. National Aeronautics and Space Administration., eds. Fuel-injector/air-swirl characterization. [Washington, DC: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаD, Cutler Andrew, and Langley Research Center, eds. Effects of jet swirl on mixing of a light gas jet in a supersonic airstream. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаExperimental Results for a High Swirl, Ultra Compact Combustor for Gas Turbine Engines. Storming Media, 2003.
Знайти повний текст джерелаЧастини книг з теми "Gas Turbine Swirl Injectors"
Ghose, Prakash, and A. Datta. "Effect of Inlet Swirl and Turbulence Levels on Combustion Performance in a Model Kerosene Spray Gas Turbine Combustor." In Lecture Notes in Mechanical Engineering, 493–504. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-7831-1_46.
Повний текст джерелаPandey, Rahul, and Krishnakant Agrawal. "Development of a Numerical Tool for Studying Turbulent Fuel–air Mixing in Swirl-Based Gas Turbine Combustion Chambers." In Lecture Notes in Mechanical Engineering, 199–211. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-6490-8_17.
Повний текст джерела"Flow And Flame Dynamics Of Lean Premixed Swirl Injectors." In Combustion Instabilities In Gas Turbine Engines, 213–76. Reston ,VA: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/5.9781600866807.0213.0276.
Повний текст джерелаPalm, R., S. Grundmann, M. Weismüller, S. Šarić, S. Jakirlić, and C. Tropea. "Experimental characterization and modelling of inflow conditions for a gas turbine swirl combustor." In Engineering Turbulence Modelling and Experiments 6, 835–44. Elsevier, 2005. http://dx.doi.org/10.1016/b978-008044544-1/50080-7.
Повний текст джерелаDomingues, Rafael, and Francisco Brójo. "Conversion of Gas Turbine Combustors to Operate with a Hydrogen-Air Mixture: Modifications and Pollutant Emission Analysis." In Hydrogen Energy - New Insights [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.106224.
Повний текст джерелаТези доповідей конференцій з теми "Gas Turbine Swirl Injectors"
Nazeer, Waseem, Kenneth Smith, Patrick Sheppard, Robert Cheng, and David Littlejohn. "Full Scale Testing of a Low Swirl Fuel Injector Concept for Ultra-Low NOx Gas Turbine Combustion Systems." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90150.
Повний текст джерелаHedman, Paul O., Thomas H. Fletcher, Stewart G. Graham, G. Wayne Timothy, Daniel V. Flores, and Jason K. Haslam. "Observations of Flame Behavior in a Laboratory-Scale Pre-Mixed Natural Gas/Air Gas Turbine Combustor From PLIF Measurements of OH." In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30052.
Повний текст джерелаWang, S., S. Y. Hsieh, and V. Yang. "Vortical dynamics and acoustic response in gas-turbine swirl-stabilized injectors." In 40th AIAA Aerospace Sciences Meeting & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-1008.
Повний текст джерелаLittlejohn, David, Robert K. Cheng, D. R. Noble, and Tim Lieuwen. "Laboratory Investigations of Low-Swirl Injectors Operating With Syngases." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-51298.
Повний текст джерелаWang, Shanwu, Shih-Yang Hsieh, and Vigor Yang. "Numerical simulation of gas turbine swirl-stabilized injector dynamics." In 39th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-334.
Повний текст джерелаBarker, A. G., and J. F. Carrotte. "The Impact of Representative Aerodynamic Flow Fields on Liquid Fuel Atomisation in Modern Gas Turbine Fuel Injectors." In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gt2014-26927.
Повний текст джерелаAjmani, Kumud, Hukam Mongia, Phil Lee, and Kathleen Tacina. "CFD-Led Designs of Pre-Filming Injectors for Gas-Turbine Combustors." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75329.
Повний текст джерелаKinoshita, Y., T. Oda, and J. Kitajima. "Low NOx Combustor Research for a Mach 3 Turbojet Concept Validation Test Results." In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-gt-153.
Повний текст джерелаMicklow, Gerald J., and Michael Benjamin. "Three Dimensional Analysis of Advanced Swirl Vane/Nozzle Assemblies." In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-226.
Повний текст джерелаLovett, Jeffery A., and Warren J. Mick. "Development of a Swirl and Bluff-Body Stabilized Burner for Low-NOx, Lean-Premixed Combustion." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-166.
Повний текст джерелаЗвіти організацій з теми "Gas Turbine Swirl Injectors"
Lightfoot, Malissa D., Stephen A. Danczyk, and Douglas G. Talley. Scaling of Gas-Centered Swirl-Coaxial Injectors. Fort Belvoir, VA: Defense Technical Information Center, October 2008. http://dx.doi.org/10.21236/ada502809.
Повний текст джерела