[1]杨向明,刘伟凯,陈林泉,等.固体燃料超燃冲压发动机原理性试验研究[J].固体火箭技术,2012,(03):319-324.[doi:10.7673/j.issn.1006-2793.2012.03.007]
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固体燃料超燃冲压发动机原理性试验研究

参考文献/References:

[1]Fry R S.A century of ramjet propulsion technology evolution[J].Journal of Propulsion and Power,2004,20(1): 27-58.
[2]刘小勇.超燃冲压发动机技术[J].飞航导弹,2003 (2): 38-42.
[3]李岩芳,郑凯斌,陈林泉.固体燃料超燃冲压发动机技术研究进展[C]//第二届冲压发动机学术会议文集,2007.
[4]Jarymowycz T A,et al.Numerical study of solid-fuel combustion under supersonic crossflows[J].Journal of Propulsion and Power,1992,8(2):346-353.
[5]Ben-Arosh R,et al.Mixing of supersonic airflow with fuel added along the wall in a sudden expansion chamber[R].AIAA 97-3241.
[6]Ben-Yakar A,et al.Experimental study of a solid fuel scramjet[R].AIAA 94-2815.
[7]Ben-Yakar A.Investigation of the combustion of solid fuel at supersonic conditions in a ramjet engine[D].M.Sc.Thesis,Dec.1995.
[8]Cohen B,et al.Experimental investigation of a supersonic combustion solid fuel ramjet[R].AIAA 97-3237.
[9]Allen C W,et al.Fuel-air injection effects on combustion in cavity-based flameholders in a supersonic flow[R].AIAA 2005-4105.
[10]Edens S G,King P I,Gruber M R,et al.Performance measurements of direct air injection in a cavity-base flameholder for a supersonic combustor[R].AIAA 2006-4861.
[11]Ben-Yakar A,et al.Investigation of a solid fuel scramjet combustor[J]. Journal of Propulsion and Power,1998,14(1): 447-455.

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更新日期/Last Update: 2012-08-01
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