| Citation: | Numerical calculation of flow characteristics of hybrid vortex reduce structure combing de-swirl inlet[J]. Journal of Aerospace Power, 2019, 34(8): 1677-1687. doi: 10.13224/j.cnki.jasp.2019.08.006
|
| [1] |
秦敏,郭文.旋转盘腔流动与换热试验准则［J］.燃气涡轮试验与研究,2014,27(2):34-36,53.QIN Min,GUO Wen.Test criteria for flow and heat transfer in rotating disk cavity［J］.Gas Turbine Test and Research,2014,27(2):34-36,53.(in Chinese)
|
| [2] |
林宏镇,汪火光,蒋章焰.高性能航空发动机传热技术.［M］.北京:国防工业出版社,2005.
|
| [3] |
赵斌,李绍斌,周盛,等.航空发动机空气系统气源引气的研究进展［J］.航空工程进展,2012,3(4):476-485.ZHAO Bin,LI Shaobin,ZHOU Sheng,et al.Research progress of air source air sequestration in aero engine air system［J］.Progress in Aeronautical Engineering,2012,3(4):476-485.(in Chinese)
|
| [4] |
FIROUZIAN M,OWEN J M,PINCOMBE J R.Flow and heat transfer in a rotating cylindrical cavity with a radial inflow of fluid:Part 1 the flow structure［J］.Heat and Fluid Flow,1985,6(4):228-234.
|
| [5] |
邓舒情.压气机旋转盘腔流动与换热性能研究［D］.北京:北京理工大学,2016.DENG Shuqing.Research on flow and heat transfer performance of compressor rotating disk cavity［D］.Beijing:Beijing Institute of Technology,2016.(in Chinese)
|
| [6] |
吴丽军,陈潇,邓双国,等.减流阻特性计算分析［J］.燃气轮机技术,2014,27(3):37-43.WU Lijun,CHEN Xiao,DENG Shuangguo,et al.Calculation and analysis of flow resistance characteristics［J］.Gas Turbine Technology,2014,27(3):37-43.(in Chinese)
|
| [7] |
DU Xiaoqin,ZHU Huiren,ZHANG Zongwei.Numerical study on varied vortex reducer configurations for the flow path optimization in compressor cavities［R］.ASME Paper GT2011-45975,2011.
|
| [8] |
CHEW J W,FARTHING P R,OWEN J M.The use of fins to reduce the pressure drop in a rotating cavity with a radial inflow［J］.Journal of Turbomachinery,1989,111(3):349-356.
|
| [9] |
DIMITRIE N,PFITZNER M.Secondary air systems in aeroengines employing vortex reducers［R］New Orleans,Louisiana,US:ASME Turbo Expo:Power for Land,Sea & Air,2001.
|
| [10] |
FRIEDL W H,PEITSCH D,NEGULESCU D,et al.Improvement of high pressure turbine air systems by de-swirl nozzles［C］∥Proceedings of the 22nd Computers and Information in Engineering Conference.Montreahl,Canada:American Society of Mechanical Engineers,2002:331-336.
|
| [11] |
PFITZNER M,WASCHKA W.Development of an aeroengine secondary air system employing vortex reducers［R］.Harogate,UK:the 22nd International Council of Aeronautical Sciences (ICAS) Congress,2000.
|
| [12] |
FARTHING P R,CHEW J W,OWEN J M.The use of de-swirl nozzles to reduce the pressure drop in a rotating cavity with radial inflow［R］.ASME Paper 89-GT-184,1989.
|
| [13] |
陈阳春,王锁芳.有去旋进气共转盘腔内流动换热数值模拟［J］.航空动力学报,2010,25(8):1746-1752.CHEN Yangchun,WANG Suofang.Numerical simulation of flow and heat transfer in a rotating disk with de-rotating air intake［J］.Journal of Aerospace Power,2010,25(8):1746-1752.(in Chinese)
|
| [14] |
赵秋月,娄德仓,郭文,等.旋转盘腔去旋系统数值模拟［J］.燃气涡轮试验与研究,2014,27(5):43-48.ZHAO Qiuyue,LOU Decang,GUO Wen,et al.Numerical simulation of rotating disk cavity derotation system［J］.Gas Turbine Experiment and Research,2014,27(5):43-48.(in Chinese)
|
| [15] |
ANDRE G,WIELAND U,ERWIN K,et al.Experimental analysis of varied vortex reducer configurations for the internal air system of jet engine gas turbines［R］.ASME Paper GT2008-50738,2008.
|
| [16] |
DLETER P,RELNHARD N.Numerical investigation of vortex reducer flows in the high compressor of modern aeroengine［R］.ASME Paper GT2002-30674,2002.
|
| [17] |
单文娟.发动机内/外部引气结构流动特性研究［D］.南京:南京航空航天大学,2014.SHAN Wenjuan.Study on flow characteristics of internal/external bleed air structure of engine［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2014.(in Chinese)
|
| [18] |
CHEN X,FENG Y,WU L.The experiment/tal investigations of centripetal air bleed with tubed vortex reducer for secondary air system in gas turbine［R］.Düsseldorf,Germany:ASME Turbo Expo,2014.
|
| [19] |
LIANG Z,LUO X,FENG Y,et al.Experimental investigation of pressure losses in a co-rotating cavity with radial inflow employing tubed vortex reducers with varied nozzles［J］.Experimental Thermal and Fluid Science,2015,66:304-315.
|
| [20] |
CFM International.LEAP-1B training manual［R］.［S.l.］:CFM International,2017.
|
| [21] |
FARTHING P R,OWEN J M.De-swirled radial inflow in a ro-tating cavity［J］.International Journal of Heat and Fluid Flow,1991,12(1):63-70.
|
| [22] |
STRELETS M.Detached eddy simulation of massively separated flows［R］.Reno,NV:the 39th Aerospace Sciences Meeting and Exhibit,2000.
|
| [23] |
FIROUZIAN M,OWEN J M,PINCOMBE J R,et al.Flow and heat transfer in a rotating cavity with a radial inflow of fluid:Part Ⅱ velocity,pressure and heat transfer measurements［J］.International Journal of Heat and Fluid Flow,1986,7(1):21-27.
|
| [24] |
黄爱霞,王锁芳.反旋进气盘腔内流动与换热的数值模拟［J］.航空动力学报,2008,23(9):1684-1688.HUANG Aixia,WANG Suofang.Numerical simulation of flow and heat transfer in a de-swirled intake disk［J］.Journal of Aerospace Power,2008,23(9):1684-1688.(in Chinese)
|
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