Aimed at the research status of the shock thrust vector control,which is limited to the mainstream and secondary flow gas as the same gas,the influence of different secondary flow gas molecular mass on thrust vector performance is investigated. First,a turbulence model described by two equations(AUSM +scheme and k-ω SST) at two-order accuracy was utilized to solve the Favre averaged three-dimensional NavierStokes equations,which simulated the complex interference inner flow field of the nozzle,and the vecto...
【基金】
国家自然科学基金(11772038)~~
【更新日期】
2018-12-11
【分类号】
V430
【正文快照】
网络出版地址:kns. cnki. net/kcms/detail/11. 2625. V. 20180419. 0951. 001. html引用格式:王晓明,刘辉,韩龙柱,等.激波诱导推力矢量喷管不同气体喷注时的性能分析[J].北京航空航天大学学报,2018,44(11):2267-2272. WANG X M,LIU H,HAN L Z,et al. Performance analysis of
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