Добірка наукової літератури з теми "Gas Turbine Engine Combustion"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся зі списками актуальних статей, книг, дисертацій, тез та інших наукових джерел на тему "Gas Turbine Engine Combustion".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Статті в журналах з теми "Gas Turbine Engine Combustion"
Agbadede, Roupa, and Biweri Kainga. "Effect of Water Injection into Aero-derivative Gas Turbine Combustors on NOx Reduction." European Journal of Engineering Research and Science 5, no. 11 (November 21, 2020): 1357–59. http://dx.doi.org/10.24018/ejers.2020.5.11.2180.
Повний текст джерелаAgbadede, Roupa, and Isaiah Allison. "Effect of Water Injection into Aero-derivative Gas Turbine Combustors on NOx Reduction." European Journal of Engineering and Technology Research 5, no. 11 (November 21, 2020): 1357–59. http://dx.doi.org/10.24018/ejeng.2020.5.11.2180.
Повний текст джерелаZhu, Dengting, Zhenzhong Sun, and Xinqian Zheng. "Turbocharging strategy among variable geometry turbine, two-stage turbine, and asymmetric two-scroll turbine for energy and emission in diesel engines." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 234, no. 7 (November 28, 2019): 900–914. http://dx.doi.org/10.1177/0957650919891355.
Повний текст джерелаChand, Dharmahinder Singh, Daamanjyot Barara, Gautam Ganesh, and Suraj Anand. "Comparison of Efficiency of Conventional Shaped Circular and Elliptical Shaped Combustor." MATEC Web of Conferences 151 (2018): 02002. http://dx.doi.org/10.1051/matecconf/201815102002.
Повний текст джерелаKru¨ger, U., J. Hu¨ren, S. Hoffmann, W. Krebs, P. Flohr, and D. Bohn. "Prediction and Measurement of Thermoacoustic Improvements in Gas Turbines With Annular Combustion Systems." Journal of Engineering for Gas Turbines and Power 123, no. 3 (October 1, 2000): 557–66. http://dx.doi.org/10.1115/1.1374437.
Повний текст джерелаJansen, M., T. Schulenberg, and D. Waldinger. "Shop Test Result of the V64.3 Gas Turbine." Journal of Engineering for Gas Turbines and Power 114, no. 4 (October 1, 1992): 676–81. http://dx.doi.org/10.1115/1.2906641.
Повний текст джерелаHutchins, T. E., and M. Metghalchi. "Energy and Exergy Analyses of the Pulse Detonation Engine." Journal of Engineering for Gas Turbines and Power 125, no. 4 (October 1, 2003): 1075–80. http://dx.doi.org/10.1115/1.1610015.
Повний текст джерелаSarkar, Asis. "A TOPSIS method to evaluate the technologies." International Journal of Quality & Reliability Management 31, no. 1 (December 20, 2013): 2–13. http://dx.doi.org/10.1108/ijqrm-03-2013-0042.
Повний текст джерелаLangston, Lee S. "Breaking the Barriers." Mechanical Engineering 134, no. 05 (May 1, 2012): 32–37. http://dx.doi.org/10.1115/1.2012-may-2.
Повний текст джерелаLangston, Lee S. "Riding the Surge." Mechanical Engineering 135, no. 05 (May 1, 2013): 37–41. http://dx.doi.org/10.1115/1.2013-may-2.
Повний текст джерелаДисертації з теми "Gas Turbine Engine Combustion"
Ahmad, 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 джерелаPerry, Matthew Vincent. "An Investigation of Lean Premixed Hydrogen Combustion in a Gas Turbine Engine." Thesis, Virginia Tech, 2009. http://hdl.handle.net/10919/43532.
Повний текст джерела
The strong lean combustion stability of hydrogen-air flames is due primarily to high reaction rates and the associated high turbulent burning velocities. While this is advantageous at low equivalence ratios, it presents a significant danger of flashbackâ the upstream propagation of the flame into the premixing deviceâ at higher equivalence ratios. An investigation has been conducted into the operation of a specific hydrogen-air premixer design in a gas turbine engine. Laboratory tests were first conducted to determine the upper stability limits of a single premixer. Tests were then carried out in which eighteen premixers and a custom-fabricated combustor liner were installed in a modified Pratt and Whitney Canada PT6A-20 turboprop engine. The tests examined the premixer and engine operability as a result of the modifications. A computer cycle analysis model was created to help analyze and predict the behavior of the modified engine and premixers. The model, which uses scaled component maps to predict off-design engine performance, was integral in the analysis of premixer flashback which limited the operation of the modified engine.
Master of Science
MacCallum, N. R. L. "Studies in gas turbine performance and in combustion." Thesis, University of Glasgow, 2000. http://theses.gla.ac.uk/5335/.
Повний текст джерелаGhulam, Mohamad. "Characterization of Swirling Flow in a Gas Turbine Fuel Injector." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563877023803877.
Повний текст джерелаPoppe, Christian. "Scalar measurements in a gas turbine combustor." Thesis, Imperial College London, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.264987.
Повний текст джерелаPeck, Jhongwoo 1976. "Development of a catalytic combustion system for the MIT Micro Gas Turbine Engine." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/28292.
Повний текст джерелаIncludes bibliographical references (p. 71-72).
As part of the MIT micro-gas turbine engine project, the development of a hydrocarbon-fueled catalytic micro-combustion system is presented. A conventionally-machined catalytic flow reactor was built to simulate the micro-combustor and to better understand the catalytic combustion at micro-scale. In the conventionally-machined catalytic flow reactor, catalytic propane/air combustion was achieved over platinum. A 3-D finite element heat transfer model was also developed to assess the heat transfer characteristics of the catalytic micro-combustor. It has been concluded that catalytic combustion in the micro-combustor is limited by diffusion of fuel into the catalyst surface. To address this issue, a catalytic structure with larger surface area was suggested and tested. It was shown that the larger surface area catalyst increased the chemical efficiency. Design guidelines for the next generation catalytic micro-combustor are presented as well.
by Jhongwoo Peck.
S.M.
Hinse, Mathieu. "Investigation of Transpiration Cooling Film Protection for Gas Turbine Engine Combustion Liner Application." Thesis, Université d'Ottawa / University of Ottawa, 2021. http://hdl.handle.net/10393/42425.
Повний текст джерелаManners, A. P. "The calculation of the flows in gas turbine combustion systems." Thesis, Imperial College London, 1998. http://hdl.handle.net/10044/1/8397.
Повний текст джерелаVillarreal, Daniel Christopher. "Digital Fuel Control for a Lean Premixed Hydrogen-Fueled Gas Turbine Engine." Thesis, Virginia Tech, 2009. http://hdl.handle.net/10919/34974.
Повний текст джерелаParallel to this study, an investigation of the existing hydrogen combustor design was performed to analyze the upper stability limits that were restricting the operability of the engine. The upstream propagation of the flame into the premixer, more commonly known as a flashback, routinely occurred at 150 shaft horsepower during engine testing. The procedures for protecting the engine from a flashback were automated within the fuel controller, significantly reducing the response time from the previous (manual) method. Additionally, protection measures were added to ensure the inter-turbine temperature of the engine did not exceed published limits. Automatic engine starting and shutdown procedures were also added to the control logic, minimizing the effort needed by the operator. The tested performance of the engine with each of the control functions demonstrated the capability of the controller.
Methods to generate an engine-specific fuel control map were also studied. The control map would not only takes into account the operability limits of the engine, but also the stability limits of the premixing devices. Such a map is integral in the complete design of the engine fuel
controller.
Master of Science
Skidmore, F. W., and n/a. "The influence of gas turbine combustor fluid mechanics on smoke emissions." Swinburne University of Technology, 1988. http://adt.lib.swin.edu.au./public/adt-VSWT20070420.131227.
Повний текст джерелаКниги з теми "Gas Turbine Engine Combustion"
Lieuwen, Timothy C., and Vigor Yang. Combustion Instabilities In Gas Turbine Engines. Reston ,VA: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/4.866807.
Повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Знайти повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Знайти повний текст джерелаCawley, James D. Phenomenological study of the behavior of some silica formers in a high velocity jet fuel burner. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.
Знайти повний текст джерелаBennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.
Знайти повний текст джерелаFuller, E. J. Integrated CFD modeling of gas turbine combustors. Washington, D. C: AIAA, 1993.
Знайти повний текст джерелаMelconian, Jerry O. Introducing the VRT gas turbine combustor. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаYoung, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.
Знайти повний текст джерелаVeres, Joseph P. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаBose, S. Materials for advanced turbine engines (MATE) project 3 design, fabrication and evaluation of an oxide dispersion strengthened sheet alloy combustor liner. [Washington, DC: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаЧастини книг з теми "Gas Turbine Engine Combustion"
Decher, Reiner. "Other Components of the Jet Engine." In The Vortex and The Jet, 125–35. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_12.
Повний текст джерелаMuduli, S. K., R. K. Mishra, and P. C. Mishra. "Computational Study of Combustion Process in a Gas Turbine Engine." In Recent Advances in Thermofluids and Manufacturing Engineering, 139–50. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-4388-1_13.
Повний текст джерелаMüller, S. H. R., B. Böhm, and A. Dreizler. "High-Speed Laser Diagnostics for the Investigation of Cycle-to-Cycle Variations of IC Engine Processes." In Flow and Combustion in Advanced Gas Turbine Combustors, 463–77. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_16.
Повний текст джерелаEckbreth, Alan C. "Laser Diagnostics for Gas Turbine Thermometry and Species Measurements." In Instrumentation for Combustion and Flow in Engines, 69–106. Dordrecht: Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-2241-9_4.
Повний текст джерелаLisanti, Joel C., and William L. Roberts. "Pulse Combustor Driven Pressure Gain Combustion for High Efficiency Gas Turbine Engines." In Combustion for Power Generation and Transportation, 127–52. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3785-6_7.
Повний текст джерелаDimitrova, D., M. Braun, J. Janicka, and A. Sadiki. "Large Eddy Simulation of Dispersed Two-Phase Flows and Premixed Combustion in IC-Engines." In Flow and Combustion in Advanced Gas Turbine Combustors, 415–44. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_14.
Повний текст джерелаBalijepalli, Ramakrishna, Abhishek Dasore, Upendra Rajak, Y. Siva Kumar Reddy, and Tikendra Nath Varma. "Design and Optimisation of Annulus Combustion Chamber of Gas Turbine Engine: An Analytical and Numerical Approach." In Lecture Notes in Mechanical Engineering, 553–67. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8341-1_47.
Повний текст джерелаSingaravelu, Balasubramanian, Sathesh Mariappan, and Avijit Saha. "Theoretical Formulation for the Investigation of Acoustic and Entropy-Driven Combustion Instabilities in Gas Turbine Engines." In Combustion for Power Generation and Transportation, 169–96. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3785-6_9.
Повний текст джерелаDascomb, John, and Anjaneyulu Krothapalli. "Hydrogen-Enriched Syngas from Biomass Steam Gasification for Use in Land-Based Gas Turbine Engines." In Novel Combustion Concepts for Sustainable Energy Development, 89–110. New Delhi: Springer India, 2014. http://dx.doi.org/10.1007/978-81-322-2211-8_6.
Повний текст джерелаScharnell, Lennart, and Stuart Sabol. "Gas Turbine Combustion." In Practical Dispute Resolution, 2–4. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-031-01493-2_2.
Повний текст джерелаТези доповідей конференцій з теми "Gas Turbine Engine Combustion"
Schlein, Barry. "Gas Turbine Combustion Efficiency." In ASME 1985 Beijing International Gas Turbine Symposium and Exposition. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-igt-121.
Повний текст джерелаHintz, Douglas E. "The 501D5A Combustion Turbine." 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-267.
Повний текст джерелаScarinci, Thomas, and John L. Halpin. "Industrial Trent Combustor — Combustion Noise Characteristics." In ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-009.
Повний текст джерелаHou, Xingxia, Shaolin Wang, Pengfu Xie, Qing Gao, Chunqing Tan, and Jianwen Wang. "CFD Simulation of Combustion in Gas Turbine Engine." In 2017 5th International Conference on Frontiers of Manufacturing Science and Measuring Technology (FMSMT 2017). Paris, France: Atlantis Press, 2017. http://dx.doi.org/10.2991/fmsmt-17.2017.170.
Повний текст джерелаGuillou, Erwann, Ephraim Gutmark, and Michael Cornwell. "Application of Flameless Combustion for Gas Turbine Engine." In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-225.
Повний текст джерелаSun, Tao, Minghui Yuan, Yuehan Xu, Guohui Wang, and Nan Ye. "Study of New Exhaust Ejector for Marine Gas Turbine." In ASME 2014 Internal Combustion Engine Division Fall Technical Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/icef2014-5482.
Повний текст джерелаNarayana Rao, Korukonda Venkata Lakshmi, B. V. S. S. S. Prasad, Ch Kanna Babu, and Girish K. Degaonkar. "Numerical and Experimental Investigations on Liner Heat Transfer in an Aero Engine Combustion Chamber." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4776.
Повний текст джерелаShouman, A. Radey, and A. R. Shouman. "The WISC Gas Turbine Engine." 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-493.
Повний текст джерелаVerma, Vishwas, Kiran Manoharan, and Jaydeep Basani. "Application of Machine Learning in Turbulent Combustion for Aviation Gas Turbine Combustor Design." In ASME 2021 Gas Turbine India Conference. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gtindia2021-76442.
Повний текст джерелаRajagopal, Manikanda, Abdullah Karimi, and Razi Nalim. "Wave-Rotor Pressure-Gain Combustion Analysis for Power Generation and Gas Turbine Applications." In ASME 2012 Gas Turbine India Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gtindia2012-9741.
Повний текст джерелаЗвіти організацій з теми "Gas Turbine Engine Combustion"
Wong, J. K. L., G. N. Banks, and H. Whaley. Durability of gas turbine engine components in a bio-fuel combustion atmosphere. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 1995. http://dx.doi.org/10.4095/304635.
Повний текст джерелаEtemad, Shahrokh, Benjamin Baird, Sandeep Alavandi, and William Pfefferle. Industrial Gas Turbine Engine Catalytic Pilot Combustor-Prototype Testing. Office of Scientific and Technical Information (OSTI), April 2010. http://dx.doi.org/10.2172/1051563.
Повний текст джерелаKorjack, T. A. A Twisted Turbine Blade Analysis for a Gas Turbine Engine. Fort Belvoir, VA: Defense Technical Information Center, August 1997. http://dx.doi.org/10.21236/ada329581.
Повний текст джерелаBattelle. Gasification Evaluation of Gas Turbine Combustion. Office of Scientific and Technical Information (OSTI), December 2003. http://dx.doi.org/10.2172/828242.
Повний текст джерелаT.E. Lippert and D.M. Bachovchin. Gas Turbine Reheat Using In-Situ Combustion. Office of Scientific and Technical Information (OSTI), March 2004. http://dx.doi.org/10.2172/993806.
Повний текст джерелаNewby, R. A., D. M. Bachovchin, and T. E. Lippert. Gas Turbine Reheat Using In-Situ Combustion. Office of Scientific and Technical Information (OSTI), April 2004. http://dx.doi.org/10.2172/993807.
Повний текст джерелаD.M. Bachovchin and T.E. Lippert. Gas Turbine Reheat Using In-Situ Combustion. Office of Scientific and Technical Information (OSTI), April 2004. http://dx.doi.org/10.2172/993808.
Повний текст джерелаD.M. Bachovchin, T.E. Lippert, and R.A. Newby P.G.A. Cizmas. GAS TURBINE REHEAT USING IN SITU COMBUSTION. Office of Scientific and Technical Information (OSTI), May 2004. http://dx.doi.org/10.2172/827534.
Повний текст джерелаCao, Yiding. Miniature Heat Pipe Devices for Gas Turbine Engine Applications. Fort Belvoir, VA: Defense Technical Information Center, December 2002. http://dx.doi.org/10.21236/ada416715.
Повний текст джерелаRoth, P. G. Probabilistic Rotor Design System (PRDS) -- Gas Turbine Engine Design. Fort Belvoir, VA: Defense Technical Information Center, December 1998. http://dx.doi.org/10.21236/ada378908.
Повний текст джерела