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喷油杆与凹腔支板稳定器近距匹配雾化特性

罗莲军 刘玉英 张文龙 季鹤鸣

罗莲军, 刘玉英, 张文龙, 季鹤鸣. 喷油杆与凹腔支板稳定器近距匹配雾化特性[J]. 航空动力学报, 2013, 28(11): 2462-2467.
引用本文: 罗莲军, 刘玉英, 张文龙, 季鹤鸣. 喷油杆与凹腔支板稳定器近距匹配雾化特性[J]. 航空动力学报, 2013, 28(11): 2462-2467.
LUO Lian-jun, LIU Yu-ying, ZHANG Wen-long, JI He-ming. Atomization characteristics of fuel injector and cavity-based strut flame stabilizer under close-range matching condition[J]. Journal of Aerospace Power, 2013, 28(11): 2462-2467.
Citation: LUO Lian-jun, LIU Yu-ying, ZHANG Wen-long, JI He-ming. Atomization characteristics of fuel injector and cavity-based strut flame stabilizer under close-range matching condition[J]. Journal of Aerospace Power, 2013, 28(11): 2462-2467.

喷油杆与凹腔支板稳定器近距匹配雾化特性

Atomization characteristics of fuel injector and cavity-based strut flame stabilizer under close-range matching condition

  • 摘要: 以水和煤油为雾化介质,采用马尔文激光粒度仪研究了来流马赫数为0.16~0.24、喷雾压差为0.30~0.90MPa、喷油杆与凹腔支板稳定器间隔为31.5mm且顺喷时液雾在轴向不同位置处的雾化特性.研究结果表明:液滴索太尔平均直径(SMD)随来流马赫数增大而减小,随喷雾压差升高而减小,但凹腔支板稳定器下游远方截面的液滴SMD在主流区对马赫数不敏感,在回流区对喷雾压差不敏感.此外,喷油杆下游液滴SMD沿轴向逐渐减小,沿径向在主流区逐渐增大,在回流区逐渐减小.

     

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出版历程
  • 收稿日期:  2012-11-03
  • 刊出日期:  2013-11-28

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