Non-stationary compressible flow in ducts with varying cross-section

被引:6
|
作者
Igra, O [1 ]
Wang, L
Falcovitz, J
机构
[1] Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn, IL-84105 Beer Sheva, Israel
[2] Hebrew Univ Jerusalem, Inst Math, IL-91904 Jerusalem, Israel
关键词
shock wave in ducts; rarefaction wave in ducts; one-dimensional duct flow; two-dimensional duct flow;
D O I
10.1243/0954410981532405
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A comparative study of the interaction of shock wave or rarefaction wave with a converging duct separating long constant cross-section segments is presented. Quasi-one-dimensional computations are compared with fully two-dimensional computations. It is observed that in some cases the two-dimensional results approach the respective one-dimensional approximations over long times, while in other cases the two-dimensional computed flow is genuinely two-dimensional and cannot be reduced to a one-dimensional equivalent. In the latter cases, significant errors are incurred by analysing the flow using the quasi-one-dimensional duct flow approximation.
引用
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页码:225 / 243
页数:19
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