Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake
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Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake
Vol. 27, Issue 6, (2012)
作者机构:
南京航空航天大学 能源与动力学院,南京,210016
作者简介:
基金信息:
DOI:
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Published:2012
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LI Yong-zhou, ZHANG Kun-yuan, NAN Xiang-jun, et al. Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake[J]. 2012, 27(6).
DOI:
LI Yong-zhou, ZHANG Kun-yuan, NAN Xiang-jun, et al. Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake[J]. 2012, 27(6).DOI:
Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake
The water-drop like shape to circular shape transition hypersonic inward turning inlet has been designed with the technology of streamline tracing and gradual change section
using an axisymmetric basic flowfield with controllable pressure rising distribution.Numerical simulations were conducted on both design point and translation point
and the comparison of performance was performed with the rectangular to circular shape transition inward turning inlet with the same design parameters.The results indicate that two types of inward turning inlet have the roughly equivalent general performance
while the water-drop like shape intake has a more uniform exit flowfield and a better starting characteristic.Furthermore
the flowfiled structure of water-drop like shape intake is asymmetric due to the asymmetric geometry shapes.