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<journal-meta>
<journal-id>International Journal of Aerospace and Lightweight Structures</journal-id>
<publication_date>2012</publication_date>
<volume>2</volume>
<issue>2</issue>
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<doi>10.3850/S2010428612000360</doi>
<article-title>An Improved Characteristic Based Split Scheme for Compressible and
Incompressible Moving Boundary Flows</article-title>
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<author>Xu Sun, Jiazhong Zhang<sup>a</sup> and Guanhua Mei</author>
<author-citation>Sun, Xu; Zhang, Jiazhong; Mei, Guanhua</author-citation>

<aff>School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, China.</aff>
<email><a href="mailto:jzzhang@mail.xjtu.edu.cn"><sup>a</sup>jzzhang@mail.xjtu.edu.cn</a></email>

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<abstract>
<title>ABSTRACT</title>
<p>An improved characteristic based split (CBS) finite element method is proposed for
both compressible and incompressible flows with moving boundaries. By this method,
the Navier-Stokes equations in the Eulerian description are taken as the governing equations
of the moving boundary problems. The segment spring analogy method is used for
mesh movement to capture the moving boundaries and preserve the mesh quality during
computation. Moreover, a projection procedure is proposed to exchange the flow information
between different meshes, and then a new CBS solution procedure is developed
for the moving mesh. Two types of moving boundary problems, including the incompressible
flow induced by an in-line oscillating circular cylinder in water at rest and the
inviscid transonic flow past a NACA 0012 airfoil with pitching oscillation, are used to
test the proposed method. In both cases, a good agreement is obtained between the
computed results and the experimental/numerical results in other literatures. Combined
with suitable solvers for solid mechanics, the present CBS finite element method could
be applied to the compressible and incompressible flow-structure interaction problems.</p><p><italic>Keywords: Characteristic based split, Finite element method, Moving boundary problem,
Spring analogy method.</italic></p>
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