Numerical investigations on thrust augmentation mechanism of single ejection driven by two detonation tubes
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Numerical investigations on thrust augmentation mechanism of single ejection driven by two detonation tubes
Vol. 26, Issue 5, (2011)
作者机构:
南京理工大学 瞬态物理国家重点实验室,南京,210094
作者简介:
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DOI:
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Published:2011
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ZHANG Huan-hao, CHEN Zhi-hua, SUN Xiao-hui. Numerical investigations on thrust augmentation mechanism of single ejection driven by two detonation tubes[J]. 2011, 26(5).
DOI:
ZHANG Huan-hao, CHEN Zhi-hua, SUN Xiao-hui. Numerical investigations on thrust augmentation mechanism of single ejection driven by two detonation tubes[J]. 2011, 26(5).DOI:
Numerical investigations on thrust augmentation mechanism of single ejection driven by two detonation tubes
and in combination with the high-resolution hybrid Roe/HLL (Harten-Lax-Van Leer) scheme and adaptive mesh refinement method
numerical simulations of single ejection driven by two pulse detonation engines (PDE) were performed.The results show the propagation processes of the ejection of the primary detonation and the secondary detonation induced inside the ejector.After two detonation waves are ejected out
they propagate in the form of unexpanded jet flow
and interact with each other at the same time
postponing the ejection time of the exhausted gases and decreasing the absorption time of ambient air.As a result
the ejection efficiency of the ejector decreases
and the numerical results agree well with corresponding experimental results.