| Citation: | LOU Yuzhu, CHEN Zhen, JIANG Shiyi. Numerical simulation on influence of thrust reverser device on aerodynamic erformance of blended-wing-body distributed propulsion system[J]. Journal of Aerospace Power, 2019, 34(10): 2211-2217. doi: 10.13224/j.cnki.jasp.2019.10.014
|
| [1] |
段静瑶,袁巍,李秋实,分布式动力系统尾缘射流与边界层抽吸数值分析［J］.航空动力学报,2015,30(3):571-579.DUAN Jingyao,YUAN Wei,LI Qiushi.Numerical investigation on trailing edge jet and boundary layer ingestion in distributed propulsion system［J］.Journal of Aerospace Power,2015,30(3):571-579.(in Chinese)
|
| [2] |
LIEBECK R H.Design of the blended wing body subsonic transport［J］.Journal of Aircraft,2004,411):10-25.
|
| [3] |
SMITH L H.Wake ingestion propulsion benefit［J］.Journal of Propulsion and Power,1993,9(1):74-82.
|
| [4] |
HILEMAN J I,SPAKOVSZKY Z S,DRELA M,et al.Airframe design for silent fuel-efficient aircraft［J］.Journal of Aircraft,2010,47(3):10-25.
|
| [5] |
KO A,LEIFSSON L T,SCHETZ J A,et al.MDO of a blended-wing-body transport aircraft with distributed propulsion［R］.AIAA-2003-6732,2003.
|
| [6] |
KIM H D,BROWN G V,FELDER J L.Distributed turbo-electric ropulsion for hybrid wing body aircraft［C］//Proceedings of 2008 International Powered Lift Conference.London:Royal Aeronautical Society,2008:1-11.
|
| [7] |
赵志高,张曙光.BWB客机经济性相关设计参数的影响分析［J］.北京航空航天大学学报,2011,37(8):937-942.ZHAO Zhigao,ZHANG Shuguang.Analysis of effects of BWB airliner design parameters on its economic profitability［J］.Journal of Beijing University of Aeronautics and Astronautics,2011,37(8):937-942.(in Chinese)
|
| [8] |
张曙光,陆艳辉,巩磊,等.250座级翼身融合无尾布局客机操稳特性设计研究［J］.航空学报,2011,32(10):1761-1769.ZHANG Shuguang,LU Yanhui,GONG Lei,et al.Research on design of stability and control of a 250-seattailless blended-wing-body civil transport aircraft［J］.Acta Aeronautica et Astronautica Sinica,2011,32(10):1761-1769.(in Chinese)
|
| [9] |
STAELENSY D,BLACKWELDER R F.Novel pitch control effectors for a blended wing body airplane in takeoff and landing configuration［R］.AIAA-2007-0068,2007.
|
| [10] |
LU Yi,ZHANG Shuguang,TANG Peng,et al.STAMP-based safety control approach for flight testing of a low-cost unmanned subscale blended-wing-body demonstrator［J］.Safety Science,2015,74:102-113.
|
| [11] |
LU Yi,ZHANG Shuguang,LIAN Hao,et al.System dynamics modeling of the safety evolution of blended-wing-body subscale demonstrator flight testing［J］.Safety Science,2016,89:219-230.
|
| [12] |
OBYE R C,HAKIM A D.Axisymmetric approach and landing thrust reverser concepts:hot flow test results［R］.AIAA 84-1176,1984.
|
| [13] |
靳宝林,邢伟红,刘殿春.飞机/发动机推进系统反推力装置［J］.航空发动机,2004,30(3):48-52.JIN Baolin,XING Weihong,LIU Dianchun.Thrust reversers of aircraft/engine propulsion systemJ］.Aeroengine,2004,30(3):48-52.(in Chinese)
|
| [14] |
王玉新,飞机发动机反推力装置的创新设计［R］.广东 深圳:大型飞机关键技术高层论坛暨中国航空学会2007年学术年会,2007.
|
| [15] |
王占学,张晨,刘春阳.抓斗式反推装置打开时反推性能参数计算［J］.航空动力学报,2009,24(10):2157-2162.WANG Zhanxue,ZHANG Chen,LIU Chunyang.Mathematical model for calculating effects of target type thrust reverser on turbofan engine performance［J］.Journal of Aerospace Power,2009,24(10):2157-2162.(in Chinese)
|
| [16] |
COOK P H,MCDONALD M A,FIRMIN M C P.Aerofoil RAE 2822:pressure distributions,and boundary layer and wake measurements［R］.AGARD Report AR 138,1979.
|
| [17] |
SPALART P R,ALLMARAS S R.A one-equation turbulence model for aerodynamic flows［J］.Recherche Aerospatiale,1994,1(1):5-21.
|
| [18] |
崔容,潘天宇,李秋实,等.边界层抽吸效应对分布式推进系统气动性能影响数值研究［J］.航空动力学报,2018,33(5):1076-1083.CUI Rong,PAN Tianyu,LI Qiushi,et al.Numerical investigation on the effects of boundary layer ingestion on aerodynamic performance of distributed propulsion system［J］.Journal of Aerospace Power,2018,33(5):1076-1083.(in Chinese)
|
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