Статті в журналах з теми "Scramjet combustor"
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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 джерелаJi, Zifei, Huiqiang Zhang, and Bing Wang. "Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 13 (February 20, 2019): 4810–24. http://dx.doi.org/10.1177/0954410019830816.
Повний текст джерелаGuimarães, Jefte Da Silva, Marco Antonio Sala Minucci, and Dermeval Carinhana Júnior. "ESTUDO DE UMA CÂMARA DE COMBUSTÃO SUPERSÔNICA USANDO UM TÚNEL DE CHOQUE." CIMATech 1, no. 7 (December 23, 2020): 126–36. http://dx.doi.org/10.37619/issn2447-5378.v7i1.297.126-136.
Повний текст джерелаCui, Tao, and Yang Ou. "Modeling of Scramjet Combustors Based on Model Migration and Process Similarity." Energies 12, no. 13 (June 30, 2019): 2516. http://dx.doi.org/10.3390/en12132516.
Повний текст джерелаHuang, Juan-Chen, Yu-Hsuan Lai, Jeng-Shan Guo, and Jaw-Yen Yang. "Simulation of Two-Dimensional Scramjet Combustor Reacting Flow Field Using Reynolds Averaged Navier-Stokes WENO Solver." Communications in Computational Physics 18, no. 4 (October 2015): 1181–210. http://dx.doi.org/10.4208/cicp.190115.210715s.
Повний текст джерелаLi, Wei Qiang, and Fei Teng Luo. "Investigation of Performance of Scramjet Combustion Used Kerosene with Clean Air." Advanced Materials Research 601 (December 2012): 294–98. http://dx.doi.org/10.4028/www.scientific.net/amr.601.294.
Повний текст джерелаYang, Jun, Xian-yu Wu, and Zhen-guo Wang. "Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor." International Journal of Aerospace Engineering 2016 (2016): 1–14. http://dx.doi.org/10.1155/2016/7604279.
Повний текст джерелаTian, Ye, Shunhua Yang, and Jialing Le. "Study on the Effect of Air Throttling on Flame Stabilization of an Ethylene Fueled Scramjet Combustor." International Journal of Aerospace Engineering 2015 (2015): 1–10. http://dx.doi.org/10.1155/2015/504684.
Повний текст джерелаKim, Min-Su, In-Hoi Koo, Keon-Hyeong Lee, Eun-Sung Lee, Hyung-Seok Han, Seung-Min Jeong, Holak Kim, and Jeong-Yeol Choi. "Experimental Study on the Ignition Characteristics of Scramjet Combustor with Tandem Cavities Using Micro-Pulse Detonation Engine." Aerospace 10, no. 8 (August 11, 2023): 706. http://dx.doi.org/10.3390/aerospace10080706.
Повний текст джерелаZhang, Linqing, Juntao Chang, Wenxiang Cai, Hui Sun, and Yingkun Li. "A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor." International Journal of Aerospace Engineering 2022 (December 30, 2022): 1–18. http://dx.doi.org/10.1155/2022/3930440.
Повний текст джерелаRouzbar, R., and S. Eyi. "Reacting flow analysis of a cavity-based scramjet combustor using a Jacobian-free Newton–Krylov method." Aeronautical Journal 122, no. 1258 (December 2018): 1884–915. http://dx.doi.org/10.1017/aer.2018.110.
Повний текст джерелаIngle, Rahul, and Debasis Chakraborty. "Numerical Simulation of Dual-Mode Scramjet Combustor with Significant Upstream Interaction." International Journal of Manufacturing, Materials, and Mechanical Engineering 2, no. 3 (July 2012): 60–74. http://dx.doi.org/10.4018/ijmmme.2012070105.
Повний текст джерелаRoga, Sukanta, and Krishna Murari Pandey. "Computational Analysis of Hydrogen-Fueled Scramjet Combustor Using Cavities in Tandem Flame Holder." Applied Mechanics and Materials 772 (July 2015): 130–35. http://dx.doi.org/10.4028/www.scientific.net/amm.772.130.
Повний текст джерелаJeong, Seung-Min, and Jeong-Yeol Choi. "Combined Diagnostic Analysis of Dynamic Combustion Characteristics in a Scramjet Engine." Energies 13, no. 15 (August 4, 2020): 4029. http://dx.doi.org/10.3390/en13154029.
Повний текст джерелаRelangi, Naresh, Lakshmi Narayana Phaneendra Peri, Caio Henrique Franco Levi Domingos, Amalia Fossella, Julia Meria Leite Henriques, and Antonella Ingenito. "Design of Supersonic and Hybrid engine based Advanced Rocket (SHAR)." IOP Conference Series: Materials Science and Engineering 1226, no. 1 (February 1, 2022): 012031. http://dx.doi.org/10.1088/1757-899x/1226/1/012031.
Повний текст джерелаFureby, Christer, Guillaume Sahut, Alessandro Ercole, and Thommie Nilsson. "Large Eddy Simulation of Combustion for High-Speed Airbreathing Engines." Aerospace 9, no. 12 (December 1, 2022): 785. http://dx.doi.org/10.3390/aerospace9120785.
Повний текст джерелаRelangi, Naresh, Antonella Ingenito, and Suppandipillai Jeyakumar. "The Implication of Injection Locations in an Axisymmetric Cavity-Based Scramjet Combustor." Energies 14, no. 9 (May 4, 2021): 2626. http://dx.doi.org/10.3390/en14092626.
Повний текст джерелаZhang, Junlong, Guangjun Feng, Guowei Luan, Hongchao Qiu, and Wen Bao. "Research on combustion performance improvement by strut/wall combined injection in scramjet combustor." Thermal Science, no. 00 (2023): 92. http://dx.doi.org/10.2298/tsci220917092z.
Повний текст джерелаOsaka, Jun, Yoshitaka Uriuda, Osamu Imamura, Kiyotaka Yamashita, Shuhei Takahashi, Mitsuhiro Tsue, and Michikata Kono. "Combustion Characteristics of Kerosene in a Scramjet Combustor." JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55, no. 637 (2007): 98–103. http://dx.doi.org/10.2322/jjsass.55.98.
Повний текст джерелаKay, I. W., W. T. Peschke, and R. N. Guile. "Hydrocarbon-fueled scramjet combustor investigation." Journal of Propulsion and Power 8, no. 2 (March 1992): 507–12. http://dx.doi.org/10.2514/3.23505.
Повний текст джерелаDeepu, M., S. S. Gokhale, and S. Jayaraj. "Numerical Modelling of Scramjet Combustor." Defence Science Journal 57, no. 4 (July 20, 2007): 367–79. http://dx.doi.org/10.14429/dsj.57.1784.
Повний текст джерелаLi, Zhen, and Hongbin Gu. "Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor." Energies 15, no. 10 (May 21, 2022): 3790. http://dx.doi.org/10.3390/en15103790.
Повний текст джерелаWei, Bao Xi, Qiang Gang, Yan Zhang, Rong Jian Liu, Liang Tian, and Xu Xu. "A Study on Performance Comparison of Integrated Aerodynamic-Ramp-Injector/ Gas-Portfire Flame Holder with Cavity." Applied Mechanics and Materials 390 (August 2013): 8–11. http://dx.doi.org/10.4028/www.scientific.net/amm.390.8.
Повний текст джерелаManna, P., and D. Chakraborty. "Numerical investigation of transverse sonic injection in a non-reacting supersonic combustor." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 219, no. 3 (March 1, 2005): 205–15. http://dx.doi.org/10.1243/095441005x30261.
Повний текст джерелаFureby, C. "Large eddy simulation modelling of combustion for propulsion applications." Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences 367, no. 1899 (July 28, 2009): 2957–69. http://dx.doi.org/10.1098/rsta.2008.0271.
Повний текст джерелаCheng, Wen Qiang, Jing Yuan Liu, and Rakesh Shrestha. "Insight in the Performance of Scramjet Combustor Based on Orthogonal Experimental Design." Advanced Materials Research 705 (June 2013): 463–67. http://dx.doi.org/10.4028/www.scientific.net/amr.705.463.
Повний текст джерелаWang, Z. P., H. B. Gu, L. W. Cheng, F. Q. Zhong, and X. Y. Zhang. "CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization." International Journal of Turbo & Jet-Engines 36, no. 1 (March 26, 2019): 45–50. http://dx.doi.org/10.1515/tjj-2016-0064.
Повний текст джерелаSuppandipillai, Jeyakumar, Jayaraman Kandasamy, R. Sivakumar, Mehmet Karaca, and Karthik K. "Numerical investigations on the hydrogen jet pressure variations in a strut based scramjet combustor." Aircraft Engineering and Aerospace Technology 93, no. 4 (April 5, 2021): 566–78. http://dx.doi.org/10.1108/aeat-08-2020-0162.
Повний текст джерелаKanda, Takeshi, Nobuo Chinzei, Kenji Kudo, Atsuo Murakami, and Tetsuo Hiraiwa. "Autoignited Combustion Testing in a Water-Cooled Scramjet Combustor." Journal of Propulsion and Power 20, no. 4 (July 2004): 657–64. http://dx.doi.org/10.2514/1.11381.
Повний текст джерелаDharavath, Malsur, P. Manna, and Debasis Chakraborty. "Thermochemical exploration of hydrogen combustion in generic scramjet combustor." Aerospace Science and Technology 24, no. 1 (January 2013): 264–74. http://dx.doi.org/10.1016/j.ast.2011.11.014.
Повний текст джерелаLi, Xiang, Qingchun Lei, Xiaocun Zhao, Wei Fan, Shuang Chen, Li Chen, Ye Tian, and Quan Zhou. "Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio." Aerospace 9, no. 4 (April 14, 2022): 214. http://dx.doi.org/10.3390/aerospace9040214.
Повний текст джерелаShi, Deyong, Wenyan Song, Jingfeng Ye, Bo Tao, Yanhua Wang, and Qiang Fu. "Experimental Investigation of Reacting Flow Characteristics in a Dual-Mode Scramjet Combustor." International Journal of Turbo & Jet-Engines 35, no. 4 (December 19, 2018): 321–30. http://dx.doi.org/10.1515/tjj-2015-0014.
Повний текст джерелаBordoloi, Namrata, Krishna Murari Pandey, and Kaushal Kumar Sharma. "Numerical Investigation on the Effect of Inflow Mach Numbers on the Combustion Characteristics of a Typical Cavity-Based Supersonic Combustor." Mathematical Problems in Engineering 2021 (September 8, 2021): 1–14. http://dx.doi.org/10.1155/2021/3526454.
Повний текст джерелаWang, Guangyu, Shijie Liu, Haoyang Peng, and Weidong Liu. "Experimental Investigation of a Cylindrical Air-Breathing Continuous Rotating Detonation Engine with Different Nozzle Throat Diameters." Aerospace 9, no. 5 (May 16, 2022): 267. http://dx.doi.org/10.3390/aerospace9050267.
Повний текст джерелаTao, C., Y. Daren, and B. Wen. "Distributed parameter control arithmetic for an axisymmetrical dual-mode scramjet." Aeronautical Journal 112, no. 1135 (September 2008): 557–65. http://dx.doi.org/10.1017/s0001924000002517.
Повний текст джерелаSarosh, Ali, Dong Yun Feng, and Muhammad Adnan. "An Aerothermodynamic Design Approach for Scramjet Combustors and Comparative Performance of Low-Efficiency Systems." Applied Mechanics and Materials 110-116 (October 2011): 4652–60. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.4652.
Повний текст джерелаZhang, Qi, Weibing Zhu, Dongchao Yang, and Hong Chen. "Numerical Investigation on Flame Stabilization of Cavity-Based Scramjet Combustor Using Compressible Modified FGM Model." International Journal of Chemical Engineering 2022 (February 8, 2022): 1–21. http://dx.doi.org/10.1155/2022/8388827.
Повний текст джерелаTian, Ye, Wen Shi, Mingming Guo, Yuan Liu, Chenlin Zhang, and Jialing Le. "Investigation of combustion characteristics in a hydrogen-fueled scramjet combustor." Acta Astronautica 186 (September 2021): 486–95. http://dx.doi.org/10.1016/j.actaastro.2021.06.021.
Повний текст джерелаTAKAHASHI, Shuhei, Kazunori WAKAI, Sadatake TOMIOKA, Mitsuhiro TSUE, and Michikata KONO. "Interaction between Combustion and Flowfield in a Rectangular Scramjet Combustor." Journal of the Japan Society for Aeronautical and Space Sciences 46, no. 538 (1998): 633–39. http://dx.doi.org/10.2322/jjsass1969.46.633.
Повний текст джерелаTakahashi, Shuhei, Kazunori Wakai, Sadatake Tomioka, Mitsuhiro Tsue, and Michikata Kono. "Effects of combustion on flowfield in a model scramjet combustor." Symposium (International) on Combustion 27, no. 2 (January 1998): 2143–50. http://dx.doi.org/10.1016/s0082-0784(98)80062-3.
Повний текст джерелаNordin-Bates, K., C. Fureby, S. Karl, and K. Hannemann. "Understanding scramjet combustion using LES of the HyShot II combustor." Proceedings of the Combustion Institute 36, no. 2 (2017): 2893–900. http://dx.doi.org/10.1016/j.proci.2016.07.118.
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