[1] |
郑严,庞重义.弹用涡喷(涡扇)发动机技术[J].飞航导弹,2001(12):43-52.
|
[2] |
郑严,庞重义.弹用涡喷(涡扇)发动机技术(续)[J].飞航导弹,2002(1):40-45.
|
[3] |
苏三买,张蕾,蔡元虎,等.弹用喷气发动机发展及关键技术分析[J].航空动力学报,2009,24(11):2410-2414. SU Sanmai,ZHANG Lei,CAI Yuanhu,et al.Microturbo engine development and key technology analysis[J].Journal of Aerospace Power,2009,24(11):2410-2414.(in Chinese)
|
[4] |
郑严.弹用涡喷发动机起动加速过程试验[J].推进技术,2000,21(4):5-8. ZHENG Yan.Starting and accelerating the missile turbojet engine by ground test[J].Journal of Propulsion Technology,2000,21(4):5-8.(in Chinese)
|
[5] |
盛德林,刘伟.巡航导弹试验故障及其分析[J].飞航导弹,1994(9):1-13.
|
[6] |
屠秋野,唐狄毅.涡扇发动机起动模型及起动控制规律研究[J].推进技术,1999,20(2):21-24. TU Qiuye,TANG Diyi.Study on startup model and startup control law of turbofan engine[J].Journal of Propulsion Technology,1999,20(2):21-24.(in Chinese)
|
[7] |
Agrawal R K,Yunis M.A generalized mathematical model to estimate gas turbine starting characteristics[R].ASME PaPer 81-GT-202,1981.
|
[8] |
YAN Deyou.A dynamic model of turbojet in starting at high altitude[R].International Society of Air-Breathing Engines,ISABE 83-7045,1983.
|
[9] |
Morita M,Sasaki M.Restart characteristics of turbofan engines[R].International Society of Air-Breathing Engines,ISABE 89-7127,1989.
|
[10] |
郑严,史新兴.弹用涡轮喷气发动机火箭橇试验研究[J].推进技术,2001,22(1):26-29. ZHENG Yan,SHI Xinxing.Investigation of rocket sled test for missile turbojet engine[J].Journal of Propulsion Technology,2001,22(1):26-29.(in Chinese)
|
[11] |
于达仁,郭钰锋,牛军,等.涡喷发动机风车起动工况的神经网络建模[J].推进技术,2001,22(3):183-186. YU Daren,GUO Yufeng,NIU Jun,et al.Turbojet modeling in wind milling based on radial basis function net works[J].Journal of Propulsion Technology,2001,22(3):183-186.(in Chinese)
|
[12] |
杨欣毅,沈伟,刘海峰,等.一种弹用涡喷发动机风车起动数值仿真方法[J].航空动力学报,2010,25(8):1776-1782. YANG Xinyi,SHEN Wei,LIU Haifeng,et al.Numerical method for modeling missile turbojet engine windmill start process[J].Journal of Aerospace Power,2010,25(8):1776-1782.(in Chinese)
|
[13] |
陈玉春,陆尧,王菊金,等.涡扇发动机炮式起动数学模型及起动特性研究[J].航空学报,2002,23(6):568-570. CHEN Yuchun,LU Yao,WANG Jujin,et al.Research on cartridge starting characteristics of turbofan engine[J].Acta Aeronautica et Astronautica Sinica,2002,23(6):568-570.(in Chinese)
|
[14] |
于军,于守志.弹用涡喷发动机飞行试验启动加速性能仿真[J].推进技术,2001,22(6):454-457. YU Jun,YU Shouzhi.Starting and accelerating model of missile turbojet engine in flight test[J].Journal of Propulsion Technology,2001,22(6):454-457.(in Chinese)
|
[15] |
牛军,于达仁,冯国泰.弹用涡喷发动机全工况闭环仿真平台[J].航空动力学报,2003,18(5):709-712. NIU Jun,YU Daren,FENG Guotai.Full process circled simulation flat of missile turbojet[J].Journal of Aerospace Power,2003,18(5):709-712.(in Chinese)
|
[16] |
江民节.炮式起动条件下的微型燃烧室烟火点火技术研究[D].南京:南京航空航天大学,2013. JIANG Minjie.Pyoroflare ignition technology research of micro combustor on cartridge starting condition[D].Nanjing:Nanjing University of Aeronautics and Astraonautics,2013.(in Chinese)
|
[17] |
刘建国.弹用涡喷发动机快速起动涡轮结构设计与分析[D].长沙:国防科学技术大学,2011. LIU Jianguo.Structure design and strength analysis of the turbine based on fast-startup of the turbojet engine[D].Changsha:Graduate School of National University of Defense Technology,2011.(in Chinese)
|
[18] |
刘建国,李小柱,冯玉红.一种小型涡喷发动机火药起动方式的研究[C]//航空学会动力分会火箭发动机专业学术交流会论文集.湖北 宜昌:中国航空学会,2006:124-127.
|
[19] |
朱榕川,代国志,贺元,等.短周期高压力试验状态下的气体流量测量[J].燃气涡轮试验与研究,2012,25(S0):1-5. ZHU Rongchuan,DAI Guozhi,HE Yuan,et al.Gas flux measurement under short period and high pressure experiment[J].Gas Turbine Experiment and Research,2012,25(S0):1-5.(in Chinese)
|
[20] |
廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005.
|