ISSN:
1573-2754
Keywords:
dusty gas
;
shock wave
;
boundary layer
;
relaxation structure
Source:
Springer Online Journal Archives 1860-2000
Topics:
Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
,
Mathematics
,
Physics
Notes:
Abstract When a dusty shock wave propagates along a flat plate, laminar boundary-layer flows are formed over the solid wall. The induced boundary layer problem is numerically investigated in the present paper. Using a two-continuum medium and twoway coupling model, the governing equations for this two-phase flow system are given and then solved by the finite difference method. The calculation results indicate that the post-shock flow field is characterized by relaxation phenomenon. The effects of the relaxation structure of the dusty shock wave on the boundary layer are discussed in detail.
Type of Medium:
Electronic Resource
URL:
http://dx.doi.org/10.1007/BF00131091
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