[1]刘瑞东,相升海,杨艳羽,等.平底翼柱型药柱燃烧规律的研究[J].固体火箭技术,2019,42(01):36-41.
 LIU Ruidong,XIANG Shenghai,YANG Yanyu,et al.Study on burning law of finocyl grain with flat head[J].Journal of Solid Rocket Technology,2019,42(01):36-41.
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平底翼柱型药柱燃烧规律的研究

参考文献/References:

[1]王元有.固体火箭发动机设计[M].北京:国防工业出版社,1984:77-102.WANG Yuanyou.Design of solid rocket motor[M].Beijing:National Defense Industry Press,1984:77-102.

[2]杨月诚.火箭发动机理论基础[M].西安:西北工业大学出版社,2010:141-162.YANG Yuecheng.Theoretical basis of rocket engine[M].Xian:Northwestern Polytechnical University Press,2010:141-162.
[3]Nisar K,LIANG Guozhu,Q Zeeshan.A hybrid optimization approach for SRM finocyl grain design[J].Chinese Journal of Aeronautics,2008,21(6):481-487.
[4]杜振宾,曹亮.变温条件下翼柱型装药受载响应分析[J].航空兵器,2014(3):32-35.DU Zhenbin,CAO Liang.Load analysis of finocyl grain under conditions of varying temperature[J].Aero Weaponry,2014(3):32-35.
[5]Wando,Taeho,Sangmin,et al.3D grain burn back analysis using the partial interface tracking method[J].Aerospace Science and Technology,2017,68:58-67.
[6]Kamran,LIANG Guozhu.Design and optimization of 3D radial slot grain configuration[J].Chinese Journal of Aeronautics,2010,23(4):409-414. [7]相升海,魏开新,李世鹏,等.开槽管型药柱燃烧规律的研究[J].固体火箭技术,2012,35(6):760-763.XIANG Shenghai,WEI Kaixin,LI Shipeng,et al.Study on burning law of slotted tube grain[J].Journal of Solid Rocket Technology,2012,35(6):760-763.
[8]苏万兴.大长径比固体火箭发动机不稳定燃烧预示及抑制方法研究[D].北京:北京理工大学,2015.SU Wanxing.Prediction and suppression methods of combustion instability in large aspect ratio solid rocket motors[D].Beijing:Beijing Institute of Technology,2015.
[9]Kamran,LIANG Guozhu,Rafique,et al.±3-sigma based design optimization of 3D Finocyl grain[J].Aerospace Science and Technology,2013,26(1):29-37.
[10]詹君彪,相升海,李世鹏,等.减面燃烧规律的药柱选用准则[J].弹箭与制导学报,2015,35(5):8591.ZHAN Junbiao,XIANG Shenghai,LI Shipeng,et al.Study on grains of regressive burning law selection criteria[J].Journal of Projectiles,Rockets,Missiles and Guidance,2015,35(5):85-91.
[11]武泽平,王东辉,胡凡,等.基于代理模型的固体火箭发动机装药设计[J].固体火箭技术,2016,39(3):321-326.WU Zeping,WANG Donghui,HU Fan,et al.Surrogate based grain design optimization for solid rocket motor[J].Journal of Solid Rocket Technology,2016,39(3):321-326.
[12]刘岩.固体火箭发动机装药燃面通用模拟算法研究[D].南京:南京理工大学,2016.LIU Yan.Research on combustion surface general simulation algorithm of solid rocket motor propellant[D].Nanjing:Nanjing University of Science and Technology,2016.
[13]Poppe,Koch,Bozic,et al.Optimization of finocyl grain geometries of solid rocket boosters[J].Clinical Lymphoma Myeloma and Leukemia,2011,11(1):143-147.
[14]Kamran,LIANG Guozhu.Design and optimization of solid rocket motor Finocyl grain using simulated annealing[J].Journal of Aerospace Power,2011,26(4):918-923.
[15]Brownlee,Kimbell.Shock propagation in solid-propellant rocket combustors[J].Aiaa Journal,2015,4(6):1132-1134.

相似文献/References:

[1]相升海,魏开新,李世鹏,等.开槽管型药柱燃烧规律的研究[J].固体火箭技术,2012,(06):760.

更新日期/Last Update: 2019-03-21
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