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逆流推力矢量喷管的非定常内流性能研究
引用本文:汪明生,杨建军.逆流推力矢量喷管的非定常内流性能研究[J].航空动力学报,2009,24(1):75-82.
作者姓名:汪明生  杨建军
作者单位:南京航空航天大学,能源与动力学院,南京,210016
摘    要:基于数值模拟方法,研究了逆流矢量喷管非定常内流性能.结果表明,在一个非定常周期内,前半个周期内附体和非附体的不同情况下,内流性能参数几乎一致,但后半个周期出现一定的差异.这是流动滞后性的表现,滞后性导致了附体不容易脱离.其起因与剪切层有关,逆流剪切层和同向流剪切层的演化过程显著不同,并且可能两者对附体的脱离起了共同的作用.最后,非定常流的结果进一步表明,逆流喷管是一种较高效率的射流式矢量喷管.

关 键 词:射流推力矢量  逆流矢晟喷管  数值模拟  非定常流动  内流性能
收稿时间:2008/3/14 0:00:00
修稿时间:8/31/2008 9:16:19 AM

Unsteady internal performance study of counterflow vectoring thrust nozzle
WANG Ming-sheng and YANG Jian-jun.Unsteady internal performance study of counterflow vectoring thrust nozzle[J].Journal of Aerospace Power,2009,24(1):75-82.
Authors:WANG Ming-sheng and YANG Jian-jun
Institution:College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;China
Abstract:Internal performance of unsteady flow of counterflow thrust vectoring nozzle has researched base on numerical simulation.The results show,in the former of half a unsteady period,the performance parameters are almost the same under attachment and deattachment cases,but have a great difference in the after of half a period.It is the representation of the flow hysteresis.The hysteresis leads the attachment of main flow difficult to depart from the wall.The origin of hysteresis may be relate to shear layer.The ...
Keywords:fluidic thrust vectoring  counterflow vetoring nozzle  numerical simulation  unsteady flow  internal performance  
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