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Статті в журналах з теми "Scramjet combustor"
Xiong, Yuefei, Jiang Qin, Kunlin Cheng, Silong Zhang, and Yu Feng. "Quasi-One-Dimensional Model of Hydrocarbon-Fueled Scramjet Combustor Coupled with Regenerative Cooling." International Journal of Aerospace Engineering 2022 (August 8, 2022): 1–14. http://dx.doi.org/10.1155/2022/9931498.
Повний текст джерелаLi, Chaolong, Zhixun Xia, Likun Ma, Xiang Zhao, and Binbin Chen. "Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity." Energies 12, no. 7 (March 31, 2019): 1235. http://dx.doi.org/10.3390/en12071235.
Повний текст джерелаAthithan, A. Antony, S. Jeyakumar, Norbert Sczygiol, Mariusz Urbanski, and A. Hariharasudan. "The Combustion Characteristics of Double Ramps in a Strut-Based Scramjet Combustor." Energies 14, no. 4 (February 5, 2021): 831. http://dx.doi.org/10.3390/en14040831.
Повний текст джерелаOuyang, Hao, Weidong Liu, and Mingbo Sun. "Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor." Scientific World Journal 2014 (2014): 1–10. http://dx.doi.org/10.1155/2014/309387.
Повний текст джерелаYang, Pengnian, Zhixun Xia, Likun Ma, BinBin Chen, Yunchao Feng, Chaolong Li, and Libei Zhao. "Influence of the Multicavity Shape on the Solid Scramjet." International Journal of Aerospace Engineering 2021 (October 26, 2021): 1–14. http://dx.doi.org/10.1155/2021/9718537.
Повний текст джерелаTahsini, AM. "Combustion efficiency and pressure loss balance for the supersonic combustor." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234, no. 6 (December 18, 2019): 1149–56. http://dx.doi.org/10.1177/0954410019895885.
Повний текст джерелаLee, Jae-Hyuk, Eun-Sung Lee, Hyung-Seok Han, Min-Su Kim, and Jeong-Yeol Choi. "A Study on a Vitiated Air Heater for a Direct-Connect Scramjet Combustor and Preliminary Test on the Scramjet Combustor Ignition." Aerospace 10, no. 5 (April 28, 2023): 415. http://dx.doi.org/10.3390/aerospace10050415.
Повний текст джерелаChen, Hao, Mingming Guo, Ye Tian, Jialing Le, Hua Zhang, and Fuyu Zhong. "Intelligent reconstruction of the flow field in a supersonic combustor based on deep learning." Physics of Fluids 34, no. 3 (March 2022): 035128. http://dx.doi.org/10.1063/5.0087247.
Повний текст джерелаYang, Pengnian, Zhixun Xia, Likun Ma, Binbin Chen, Yunchao Feng, Chaolong Li, and Libei Zhao. "Direct-Connect Test of Solid Scramjet with Symmetrical Structure." Energies 14, no. 17 (September 6, 2021): 5589. http://dx.doi.org/10.3390/en14175589.
Повний текст джерелаZhao, Zhelong, and Xianyu Wu. "Control Oriented Model for Expander Cycle Scramjet." MATEC Web of Conferences 257 (2019): 01004. http://dx.doi.org/10.1051/matecconf/201925701004.
Повний текст джерелаДисертації з теми "Scramjet combustor"
Rowan, Scott A. "Viscous drag reduction in a scramjet combustor /." St. Lucia, Qld, 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17438.pdf.
Повний текст джерелаStouffer, Scott David. "The effect of flow structure on the combustion and heat transfer in a scramjet combustor." Diss., Virginia Tech, 1995. http://hdl.handle.net/10919/39116.
Повний текст джерелаMundis, Nathan L. "Magnetohydrodynamic power generation in a scramjet using a post combustor generator." Diss., Rolla, Mo. : University of Missouri-Rolla, 2007. http://scholarsmine.umr.edu/thesis/pdf/Mundis_09007dcc8043ee98.pdf.
Повний текст джерелаVita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed March 25, 2008) Includes bibliographical references (p. 95-97).
Corbin, Christopher Ryan. "Design and Analysis of a Mach 3 Dual Mode Scramjet Combustor." Wright State University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=wright1208370076.
Повний текст джерелаMilligan, Ryan Timothy. "DUAL MODE SCRAMJET: A COMPUTATIONAL INVESTIGATION ON COMBUSTOR DESIGN AND OPERATION." Wright State University / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=wright1251725076.
Повний текст джерелаMalo-Molina, Faure Joel. "Numerical study of innovative scramjet inlets coupled to combustors using hydrocarbon-air mixture." Diss., Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/33906.
Повний текст джерелаGriffiths, Alan David, and alan griffiths@anu edu au. "Development and demonstration of a diode laser sensor for a scramjet combustor." The Australian National University. Faculty of Science, 2005. http://thesis.anu.edu.au./public/adt-ANU20051114.132736.
Повний текст джерелаGriffiths, Alan David. "Development and demonstration of a diode laser sensor for a scramjet combustor /." View thesis entry in Australian Digital Theses, 2005. http://thesis.anu.edu.au/public/adt-ANU20051114.132736/index.html.
Повний текст джерелаEtheridge, Steven J. "Effect of Flow Distortion on Fuel Mixing and Combustion in an Upstream-Fueled Cavity Flameholder for a Supersonic Combustor." University of Cincinnati / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1353100774.
Повний текст джерелаMcDaniel, Keith Scott. "Three Dimensional Simulation of Time-Dependent Scramjet Isolator /Combustor Flowfields Implemented on Parallel Architectures." NCSU, 2001. http://www.lib.ncsu.edu/theses/available/etd-20001228-204538.
Повний текст джерелаMcDaniel, Keith S. Three Dimensional Simulation of Time-DependentScramjet Isolator / Combustor Flowfields Implemented onParallel Architectures, ( Under the directions of Dr. J. R. Edwards). The development of a parallel Navier-Stokes solver for computing time-dependent,three-dimensional reacting flowfields within scramjet (supersonic combusting ramjet)engines is presented in this work. The algorithm combines low-diffusion upwinding methods, timeaccurate implicit integration techniques, and domain decomposition strategies to yield an effectiveapproach for large-scale simulations. The algorithm is mapped to a distributed memoryIBM SP-2 architecture and a shared memory Compaq ES-40 architecture using the MPI-1 message-passingstandard. Two and three-dimensional simulations of time-dependent hydrogen fuel injection into a modelscramjet isolator / combustor configuration at two equivalence ratios are performed. Thesesimulations are used to gain knowledge of engine operability, inlet performance, isolatorperformance, fuel air mixing, flame holding, mode transition, and engine unstart.Results for an injection at a ratio of 0.29 show qualitative agreement withexperiment for the two-dimensional case, but revealed a slow progression towardengine unstart for the three-dimensional case. Injection at an equivalence ratio of 0.61resulted in engine unstart for both two-dimensional and three-dimensional cases.Engine unstart for the three-dimensional case occurs as a response to the formation and growthof large pockets of reversed flow along the combustor side wall. These structuresdevelop at an incipient pressure above 154 kPa and result in significant blockage of the core flow,additional compression, and chemical reaction within the boundary layer. All of these factors promotea much more rapid unstart as compared with the two-dimensional case.
Книги з теми "Scramjet combustor"
Center, Langley Research, ed. HYPULSE combustor analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаCenter, Langley Research, ed. HYPULSE combustor analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаJacobs, P. A. Preliminary calibration of a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1991.
Знайти повний текст джерелаJacobs, P. A. Flow establishment in a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.
Знайти повний текст джерелаA, Jacobs Peter, and Langley Research Center, eds. Flow establishment in a generic scramjet combustor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаA, Jacobs Peter, and Langley Research Center, eds. Preliminary calibration of a generic scramjet combustor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [1991], 1991.
Знайти повний текст джерелаDash, Sanford M. Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1: Combustor and nozzle models. New York: AIAA, 1986.
Знайти повний текст джерела1934-, Hoffman Joe D., and United States. National Aeronautics and Space Administration., eds. Hypervelocity scramjet combustor-nozzle, analysis and design: Final report for NASA grant NAG-1-854 for the period 15 February 1988 to 31 December 1991. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаT, Curran E., and Murthy S. N. B, eds. Scramjet propulsion. Reston, Va: American Institute of Aeronautics and Astronautics, 2000.
Знайти повний текст джерелаSchetz, Joseph A. Studies in scramjet flowfields. [S.l.]: American Institute of Aeronautics and Astronautics, 1987.
Знайти повний текст джерелаЧастини книг з теми "Scramjet combustor"
Morgan, R. G., and F. Zander. "Radiatively cooled scramjet combustor." In Shock Waves, 1135–40. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-85181-3_55.
Повний текст джерелаSwithenbank, J., B. C. R. Ewan, S. B. Chin, L. Shao, and Y. Wu. "Mixing Power Concepts in Scramjet Combustor Design." In ICASE/NASA LaRC Series, 531–84. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2884-4_26.
Повний текст джерелаZheng, Z. H., and J. L. Le. "Massively parallel computation of three-dimensional scramjet combustor." In Shock Waves, 897–902. Berlin, Heidelberg: Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/978-3-540-27009-6_136.
Повний текст джерелаDrummond, J. P. "Discussion on Mixing Power Concepts in Scramjet Combustor Design." In ICASE/NASA LaRC Series, 585–87. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2884-4_27.
Повний текст джерелаChevalier, Alain, Marc Bouchez, Dominique Bouchaud, Isabelle Auneau, and Nicole Montmayeur. "An industrial point of view on scramjet combustor design." In Fluid Mechanics and Its Applications, 163–72. Dordrecht: Springer Netherlands, 1997. http://dx.doi.org/10.1007/978-94-011-5432-1_13.
Повний текст джерелаDu, Jinfeng, Chun Guan, Yuchun Chen, Haomin Li, and Zhihua Wang. "Analysis of Overall Performance of Multi-stage Combustor Scramjet Engine." In Lecture Notes in Electrical Engineering, 1835–46. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_147.
Повний текст джерелаLiang, J. H., and C. Y. Wang. "Numerical Simulations of Tranverse Jet Reacting Flows in Scramjet Combustor." In Computational Mechanics ’95, 923–28. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79654-8_150.
Повний текст джерелаNaveen, K., Mukesh Kapoor, M. S. Prasad, and S. Arunvinthan. "Design and Analysis of a Novel Cloverleaf Combustor for Scramjet Engine." In Lecture Notes in Mechanical Engineering, 51–63. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-6469-3_5.
Повний текст джерелаPurwar, Anupam. "Thermo-Structural Design of Strut Based Flame Holder for Scramjet Combustor." In Research into Design for Communities, Volume 1, 105–15. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3518-0_10.
Повний текст джерелаShin, Junsu, and Hong-Gye Sung. "Comparison of Hybrid RANS/LES Methods for Supersonic Combustion in a Model Scramjet Combustor." In Progress in Hybrid RANS-LES Modelling, 233–42. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-70031-1_19.
Повний текст джерелаТези доповідей конференцій з теми "Scramjet combustor"
Zander, Fabian, and Richard Morgan. "Composite Scramjet Combustor." In 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-7354.
Повний текст джерелаChen, Yen-Sen, Y. Y. Lian, Bill Wu, and J. S. Wu. "Scramjet Combustor Computational Modeling." In 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-5386.
Повний текст джерелаMathur, T., K. C. Lin, P. Kennedy, M. Gruber, J. Donbar, T. Jackson, and F. Billig. "Liquid JP-7 combustion in a scramjet combustor." In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3581.
Повний текст джерелаBouchez, Marc, Nicole Montmayeur, Christophe Leboucher, and Michel Souchet. "Scramjet combustor design in France." In International Aerospace Planes and Hypersonics Technologies. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-6094.
Повний текст джерелаKAY, I., W. PESCHKE, and R. GUILE. "Hydrocarbon-fueled scramjet combustor investigation." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2337.
Повний текст джерелаAbdel-Salam, Tarek, Surundra Tiwari, and Tajeldin Mohieldin. "Study of Supersonic Combustion Characteristics in a Scramjet Combustor." In 16th AIAA Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-3550.
Повний текст джерелаAbdel-Salam, T., S. Tiwari, and T. Mohieldin. "Dual-mode flowfield in scramjet combustor." In 35th AIAA Thermophysics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-2966.
Повний текст джерелаIngenito, Antonella, Claudio Bruno, and Donato Cecere. "LES of the Hyshot Scramjet Combustor." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-758.
Повний текст джерелаLadeinde, Foluso. "Pressure Effects in a Scramjet Combustor." In AIAA Propulsion and Energy 2021 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3534.
Повний текст джерелаUhrig, Gilles, and Jean Michel Larrieu. "Towards An All-Composite SCRAMJET Combustor." In 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-3883.
Повний текст джерелаЗвіти організацій з теми "Scramjet combustor"
Brown, Michael S., Skip Williams, Chadwick D. Lindstrom, and Dominic L. Barone. Progress in Applying Tunable Diode Laser Absorption Spectroscopy to Scramjet Isolators and Combustors. Fort Belvoir, VA: Defense Technical Information Center, May 2010. http://dx.doi.org/10.21236/ada522512.
Повний текст джерелаClemens, Noel T. Experimental/Computational Studies of Combined-Cycle Propulsion: Physics and Transient Phenomena in Inlets and Scramjet Combustors. Fort Belvoir, VA: Defense Technical Information Center, May 2010. http://dx.doi.org/10.21236/ada525600.
Повний текст джерелаBoles, John, and Ryan Milligan. Technology for Sustained Supersonic Combustion Task Order 0006: Scramjet Research with Flight-Like Inflow Conditions. Fort Belvoir, VA: Defense Technical Information Center, January 2013. http://dx.doi.org/10.21236/ada586382.
Повний текст джерела