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李建平

西北工業大學副教授

李徠建平,博士、副教授,西北工業大學動力與能源學院副教授

人物經歷


學習經歷

2003年7月,西北工業大學動力與能源學院,獲環境科學學士學位;
2006年4月,西北工業大學動力與能源學院,獲熱能工程碩士學位;
2009年11月,西北工業大學動力與能源學院,獲航空宇航推進理論與工程博士學位。

工作經歷

2009年12月至2011年11月,西北工業大學動力與能源學院,博士后流動站;
出站后留校工作,先後任講師、副教授。

主講課程


《新概念航空航天推進技術》,《超音速燃燒衝壓發動機原理》,《超音速燃燒理論基礎》等。

獲獎記錄


兩項科研成果分別獲2007年和2008年國防科技進步三等獎,主要完成人。

研究方向


超燃衝壓發動機總體性能及優化設計,超音速燃燒理論與試驗,超音速燃燒實驗技術和測量技術,超燃衝壓發動機控制規律設計。

科研項目


先後主持中國博士后基金、航天支撐基金、航空科學基金、西工大基礎研究基金等項目,主持XX國家重大專項兩項,參加XX國家重大專項五項。

學術成果


發表學術論文十多篇。
Li Jianping,Song Wenyan, Han Xiaobao, Fu Qiang,Design and experiments of the fuel control method for the scramjet engine,SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES,VOL.40,No.1,155-171頁,2015(SCI:000351208500010,EI:20150800550019)
LiJian-ping,Song Wen-yan, Liu Xin,Scramjet Propulsive Flowpath Design and Numerical Simulation,INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,VOL.30,No.2,105-109頁,2014(SCI:000337349700002,EI:20142917956757)
li Jianping,Song Wenyan, Luo Feiteng, Shi Deyong, Experimental investigation of vitiation effects on supersonic combustor performance,Acta Astronautica,VOL.96, 296–302頁,2014,(SCI:000331666400029,EI: 20140417225498);
李建平,宋文艷,羅飛騰,陳亮, H2O/CO2污染對煤油燃料超聲速燃燒影響數值研究,推進技術,Vol.34, No.4, 562–571頁,2013(EI: 20132016340766);
李建平,宋文艷,鄭亞明,羅飛騰,超燃衝壓發動機一體化設計及數值模擬研究,航空動力學報,Vol.24,No.4,911~917頁,2009(EI:20091912073429);
李建平,宋文艷,肖隱利,超燃衝壓發動機/機體一體化優化設計,航空動力學報,Vol.26,No.4,874~879頁,2011(EI:201120112714112331);
徠LI jian-ping, SONG Wen-yan , LUO Fei-teng .The Influence of Geometric Parameters upon Nozzle Performance in Scramjet,Chinese Journal of Aeronautics, Vol.21,No.6,2008(SCI: 000262120500004,EI: 20090311857247);
LI jian-ping, SONG Wen-yan ,XING Ying.Research on nozzle performance in scramjet,5th International Conference on Fluid Mechanics ,Shanghai, PEOPLES R CHINA, AUG 15-19,2007(ISTP:000254042000089);
LI Jian-ping, SONG Wen-yan, Luo Fei-teng ,Research on scramjet full flowpath design and numerical simulation,the Preceedings of 2010 Asia-pacific International Syposium on Aperspace Technology, Xi’an, PEOPLES R CHINA, SEP 15-19,2010,p1135-1138(ISTP:000288362800270,EI:20145000304802);
LI Jian-ping, SONG Wen-yan, WANG Wei, Luo Fei-teng ,Research on the optimization design of variable-geometry scramjet,the Preceedings of 2010 Asia-pacific International Syposium on Aperspace Technology, Xi’an, PEOPLES R CHINA, SEP 15-19,2010,p1088-1091(ISTP:000288362800259,EI:20145000304791)。
1.
Li Jianping,Song Wenyan, Han Xiaobao, Fu Qiang,Design and experiments of the fuel control method for the scramjet engine,SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES,VOL.40,No.1,155-171頁,2015(SCI:000351208500010,EI:20150800550019)
2.
LiJian-ping,Song Wen-yan, Liu Xin,Scramjet Propulsive Flowpath Design and Numerical Simulation,INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,VOL.30,No.2,105-109頁,2014(SCI:000337349700002,EI:20142917956757)
3.
li Jianping,Song Wenyan, Luo Feiteng, Shi Deyong, Experimental investigation of vitiation effects on supersonic combustor performance,Acta Astronautica,VOL.96, 296–302頁,2014,(SCI:000331666400029,EI: 20140417225498);
4.
李建平,宋文艷,羅飛騰,陳亮, H2O/CO2污染對煤油燃料超聲速燃燒影響數值研究,推進技術,Vol.34, No.4, 562–571頁,2013(EI: 20132016340766);
5.
李建平,宋文艷,鄭亞明,羅飛騰,超燃衝壓發動機一體化設計及數值模擬研究,航空動力學報,Vol.24,No.4,911~917頁,2009(EI:20091912073429);
6.
李建平,宋文艷,肖隱利,超燃衝壓發動機/機體一體化優化設計,航空動力學報,Vol.26,No.4,874~879頁,2011(EI:201120112714112331);
7.
LI jian-ping, SONG Wen-yan , LUO Fei-teng .The Influence of Geometric Parameters upon Nozzle Performance in Scramjet,Chinese Journal of Aeronautics, Vol.21,No.6,2008(SCI: 000262120500004,EI: 20090311857247);
8.
LI jian-ping, SONG Wen-yan ,XING Ying.Research on nozzle performance in scramjet,5th International Conference on Fluid Mechanics ,Shanghai, PEOPLES R CHINA, AUG 15-19,2007(ISTP:000254042000089);
9.
LI Jian-ping, SONG Wen-yan, Luo Fei-teng ,Research on scramjet full flowpath design and numerical simulation,the Preceedings of 2010 Asia-pacific International Syposium on Aperspace Technology, Xi’an, PEOPLES R CHINA, SEP 15-19,2010,p1135-1138(ISTP:000288362800270,EI:20145000304802);
10.
LI Jian-ping, SONG Wen-yan, WANG Wei, Luo Fei-teng ,Research on the optimization design of variable-geometry scramjet,the Preceedings of 2010 Asia-pacific International Syposium on Aperspace Technology, Xi’an, PEOPLES R CHINA, SEP 15-19,2010,p1088-1091(ISTP:000288362800259,EI:20145000304791)。