Citation: | ZHAO J, LIU C Y, WANG Y F, et al. Research on calibration method of aeroengine temperature rise combustion efficiency[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(5): 49-55. DOI: 10.11729/syltlx20220139 |
[1] |
张宝诚. 航空发动机燃烧室的现状和发展[J]. 航空发动机, 2013, 39(6): 67–73.
ZHANG B C. Status and development of aeroengine combustors[J]. Aeroengine, 2013, 39(6): 67–73.
|
[2] |
刁瑶朋, 柴昕. 放大型喷嘴对航空发动机燃烧性能的影响[J]. 沈阳航空航天大学学报, 2015, 32(2): 38–42.
DIAO Y P, CHAI X. Effect of flux magnified injector on aero-engine combustion performance[J]. Journal of Shenyang Aerospace Ace University, 2015, 32(2): 38–42.
|
[3] |
门玉宾, 柴昕, 张羽鹏, 等. 整机条件下主燃烧室参数测量研究[J]. 航空发动机, 2015, 41(2): 81–84. DOI: 10.13477/j.cnki.aeroengine.2015.02.017
MEN Y B, CHAI X, ZHANG Y P, et al. Parameters measurement investigation of a combustor in engine testing[J]. Aeroengine, 2015, 41(2): 81–84. doi: 10.13477/j.cnki.aeroengine.2015.02.017
|
[4] |
Mongia H C. TAPS: A 4th generation propulsion combustor technology for low emissions[R]. AIAA-2003-2657, 2003.
|
[5] |
LEPICOVSKY J. Effects of a rotating aerodynamic probe on the flow field of a compressor rotor[R]. NASA/CR-2008-215215, 2008
|
[6] |
VAN ERP C A, RICHMAN M H. Technical challenges associated with the development of advanced combustion systems [C]// Proc of the Applied Vehicle Technology Panel Symposium Organized by the Former AGARD Propulsion and Energetics Panel. 1998: 124-132.
|
[7] |
MEYER T R, BROWN M S, FONOV S, et al. Optical diagnostics and numerical characterization of a trapped-vortex combustor[R]. AIAA-2002-3863, 2002. doi: 10.2514/6.2002-3863
|
[8] |
李亚娟, 王明瑞, 葛新, 等. 基于燃气分析法的航空发动机燃烧室性能研究[J]. 航空发动机, 2016, 42(1): 37–41. DOI: 10.13477/j.cnki.aeroengine.2016.01.008
LI Y J, WANG M R, GE X, et al. Research on aeroengine combustor performance based on gas analysis method[J]. Aeroengine, 2016, 42(1): 37–41. doi: 10.13477/j.cnki.aeroengine.2016.01.008
|
[9] |
王明瑞, 肖阳, 韩冰, 等. 航空燃气涡轮发动机燃气分析测试及计算方法[J]. 航空动力学报, 2015, 30(11): 2568–2574. DOI: 10.13224/j.cnki.jasp.2015.11.002
WANG M R, XIAO Y, HAN B, et al. Gas analysis test and calculation method of aeroengine[J]. Journal of Aerospace Power, 2015, 30(11): 2568–2574. doi: 10.13224/j.cnki.jasp.2015.11.002
|
[10] |
赵俭. 基于双热传导方程的高温燃气温度传感器设计方法[J]. 计量学报, 2022, 43(2): 215–221. DOI: 10.3969/j.issn.1000-1158.2022.02.13
ZHAO J. Design method of high gas temperature sensor based on double heat conduction equation[J]. Acta Metrologica Sinica, 2022, 43(2): 215–221. doi: 10.3969/j.issn.1000-1158.2022.02.13
|
[11] |
CHERNOVSKY M, ATREYA A, SACKSTEDER K. Transient measurements of temperature and radiation intensity in spherical microgravity diffusion flames[C]//Proc of the 44th AIAA Aerospace Sciences Meeting and Exhibit. 2006. doi: 10.2514/6.2006-746
|
[12] |
吴朋, 林涛. 基于QGA-SVM的铠装热电偶传感器辨识建模研究[J]. 仪器仪表学报, 2014, 35(2): 343–349. DOI: 10.3969/j.issn.0254-3087.2013.04.019
WU P, LIN T. Research on identification modeling of sheathed thermocouple sensor based on hybrid QGA-SVM[J]. Chinese Journal of Scientific Instrument, 2014, 35(2): 343–349. doi: 10.3969/j.issn.0254-3087.2013.04.019
|
[13] |
廖理. 热学计量[M]. 北京: 原子能出版社, 2002: 714-717.
|
[14] |
杨兆欣, 顾正华, 张文清, 等. 基于热电偶的低速风洞气流温度误差补偿方法[J]. 仪器仪表学报, 2022, 43(5): 68–76. DOI: 10.19650/j.cnki.cjsi.J2108335
YANG Z X, GU Z H, ZHANG W Q, et al. The error compensation method of the low-speed wind tunnel flow temperature based on the thermocouple[J]. Chinese Journal of Scientific Instrument, 2022, 43(5): 68–76. doi: 10.19650/j.cnki.cjsi.J2108335
|
[15] |
曾祥辉, 齐乐华, 肖渊, 等. 均匀液滴喷射过程中温度的测量及计算[J]. 仪器仪表学报, 2011, 32(1): 93–98. DOI: 10.3321/j.issn:0254-3087.2009.03.027
ZENG X H, QI L H, XIAO Y, et al. Droplet temperature measurement and calculation during spray process[J]. Chinese Journal of Scientific Instrument, 2011, 32(1): 93–98. doi: 10.3321/j.issn:0254-3087.2009.03.027
|
[16] |
ITO Y, INOKURA N, NAGASAKI T. Conjugate heat transfer in air-to-refrigerant airfoil heat exchangers[J]. ASME Journal of Heat and Transfer, 2014, 136(8): 081703. doi: 10.1115/1.4027554
|
[17] |
DUKHAN N, AL-RAMMAHI M A, SULEIMAN A S. Fluid temperature measurements inside metal foam and comparison to Brinkman-Darcy flow convection analysis[J]. International Journal of Heat and Mass Transfer, 2013, 67: 877–884. doi: 10.1016/j.ijheatmasstransfer.2013.08.055
|
[18] |
ZHENG C H, CHENG L M, SAVELIEV A, et al. Gas and solid phase temperature measurements of porous media combustion[J]. Proceedings of the Combustion Institute, 2011, 33(2): 3301–3308. doi: 10.1016/j.proci.2010.05.037
|
[19] |
GUMEN V, ILLYAS B, MAQSOOD A, et al. High-temperature thermal conductivity of ceramic fibers[J]. Journal of Materials Engineering and Performance, 2001, 10(4): 475–478. doi: 10.1361/105994901770344917
|
[20] |
STOUFFER S, BALLAL D, ZELINA J, et al. Development and combustion performance of a high pressure WSR and TAPS combustor[R]. AIAA-2005-1416, 2005.
|
[21] |
赵俭, 杨永军. 气流温度测量技术[M]. 北京: 中国质检出版社, 2017: 98-106.
|