|
[1] 高贤智, 李锋, 郭大鹏.
超高温升中心分级燃烧室设计及计算分析[J]. 航空发动机,
2015, 41(1): 9-15. DOI:10.13477/j.cnki.aeroengine.2015.01.002.
[2] 于建桥, 王成军, 里海洋,
等. 主燃级旋流器对中心分级燃烧室出口性能的影响[J]. 沈阳航空航天大学学报,
2023, 40(1): 22-30. DOI:10.3969/j.issn.2095-1248.2023.01.004.
[3] 李乐, 索建秦, 郑龙席.
旋向对中心分级燃烧室流场及温度场影响研究[J]. 西北工业大学学报,
2020, 38(6): 1198-1209. DOI:10.3969/j.issn.1000-2758.2020.06.008.
[4] 于建桥, 王成军, 里海洋,
等. 旋流器结构特征参数对中心分级燃烧室温度场的影响[J]. 燃气涡轮试验与研究,
2023, 36(2): 14-21. DOI:10.3969/j.issn.1672-2620.2023.02.003.
[5] 刘富强, 房爱兵, 崔玉峰, 等. 回流环形燃烧室出口温度场的试验[J]. 航空动力学报, 2012, 27(1): 48-54. DOI:10.13224/j.cnki.jasp.2012.01.014.
[6] 严友谊. 进口气流预旋对燃烧室出口温度场影响研究[D]. 上海: 上海交通大学,
2017.
[7] 伍智. 高温升燃烧室出口温度场掺混孔调控技术研究[D]. 南京: 南京航空航天大学,
2013.
[8] 吴超, 徐让书, 蒲宁, 等. 某型航空发动机燃烧室出口温度场数值模拟[J]. 沈阳航空工业学院学报, 2009, 26(2): 1-4. DOI:10.3969/j.issn.2095-1248.2009.02.001.
[9] BAIN D, SMITH C,
HOLDEMAN J. CFD mixing analysis of jets injected from straight and slanted slotsinto confined crossflow in rectangular ducts[C]//28th Joint Propulsion Conference and Exhibit. Nashville, TN, USA. AIAA, 1992: AIAA1992-3087.. DOI:10.2514/6.1992-3087.
[10] HOLDEMAN J D, CHANG C T. Mixing of
multiple jets with a confined subsonic crossflow: Part III—The effects of air
preheat and number of orifices on flow and emissions in an RQL mixing
section[R]. NASA Technical Memorandum TM-2008-215151, 2008.
[11] HOLDEMAN J, CLISSET J R, MODER J.
Spreadsheet calculations for jets in crossflow: Opposed rows of inline and
staggered holes and single and opposed rows with alternating hole sizes[R].
NASA Technical Memorandum TM-2010-216100, 2011.
[12] ZHANG M, WU H, WANG
H. Numerical prediction of NOxemission and exit temperature pattern
in a model staged lean premixed prevaporized combustor[C]//ASME Turbo Expo 2013: Turbine Technical
Conference and Exposition,
2013
DOI:10.1115/GT2013-95235.
[13] SHANG M T, LU S Q,
MAO R H. Numerical investigation of the effects of dilution hole geometry on
the exit temperature profile and emissions of an aero-engine LPP combustor[C]//ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, 2013 DOI:10.1115/GT2013-95395.
[14] ELKADY A M. Experimental investigation of aerodynamics,
combustion, and emissions characteristics within the primary zone of a gas
turbine combustor [D]. Cincinnati: University of Cincinnati, 2006.
[15] ELKADY A, JENG S M,
MONGIA H. The influence of primary air jets on flow and pollutant emissions
characteristics within a model gas turbine combustor[C]//44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada. AIAA, 2006: AIAA2006-544.. DOI:10.2514/6.2006-544.
[16] 于建桥. 中心分级燃烧室燃烧流场性能的研究[D]. 沈阳: 沈阳航空航天大学, 2023. DOI:10.27324/d.cnki.gshkc.2023.000294.
[17] 江平, 何小民. 仅值班供油时斜流驻涡燃烧室出口温度分布特性研究[J]. 推进技术, 2021, 42(6): 1303-1311.
DOI:10.13675/j.cnki.tjjs.190876.
[18] 申力鑫. 掺混孔几何参数对燃烧室出口特性的影响[D]. 沈阳: 沈阳航空航天大学, 2018.
[19] 杨思恒, 王建臣, 张弛, 等. 三头部中心分级燃烧室出口温度分布研究[J]. 工程热物理学报, 2021, 42(10):
2737-2748. |