Preliminary investigation on parametric design method of thetwo dimensional hypersonic inlet
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Preliminary investigation on parametric design method of thetwo dimensional hypersonic inlet
Vol. 22, Issue 1, (2007)
作者机构:
国防科学技术大学 航天与材料工程学院,湖南,长沙,410073
作者简介:
基金信息:
DOI:
CLC:
Published:2007
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FAN Xiao-qiang, LI Hua, LI Xiao-yu, et al. Preliminary investigation on parametric design method of thetwo dimensional hypersonic inlet[J]. 2007, 22(1).
DOI:
FAN Xiao-qiang, LI Hua, LI Xiao-yu, et al. Preliminary investigation on parametric design method of thetwo dimensional hypersonic inlet[J]. 2007, 22(1).DOI:
Preliminary investigation on parametric design method of thetwo dimensional hypersonic inlet
A parametric design method of the two-dimensional hypersonic inlet was established.By analyzing the restriction and sensitivity of the parameters which affect the inlet performance or configuration
five basic geometric parameters were selected for the parametric inlet design.It is indicated that the key performance and the configuration of the inlet are sensitive to the basic parameters selected.The parametric design method provides a practical way for the optimization design of the two-dimensional inlet.