<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.0//EN" "http://www.ncbi.nlm.nih.gov:80/entrez/query/static/PubMed.dtd">
<ArticleSet>
<Article>
<Journal>
<PublisherName>Science and Education Publishing</PublisherName>
<JournalTitle>Journal of Mathematical Sciences and Applications</JournalTitle>
<Volume>1</Volume>
<Issue>1</Issue>
<PubDate PubStatus="epublish">
<Year>2013</Year>
<Month>03</Month>
<Day>25</Day>
</PubDate>
</Journal>
<ArticleTitle>Assessment of Air Flow over an Equilateral Triangular Obstacle in a Horizontal Channel Using FVM</ArticleTitle>
<FirstPage>12</FirstPage>
<LastPage>16</LastPage>
<Language>EN</Language>
<AuthorList>
<Author>
<FirstName>Roya</FirstName>
<LastName>Shademani</LastName>
</Author>
<Author>
<FirstName>Parviz</FirstName>
<LastName>Ghadimi</LastName>
<Affiliation>Department of Marine Technology, Amirkabir University of Technology, Tehran, Iran</Affiliation>
</Author>
<Author>
<FirstName>Rahim</FirstName>
<LastName>Zamanian</LastName>
</Author>
<Author>
<FirstName>Abbas</FirstName>
<LastName>Dashtimanesh</LastName>
</Author>

</AuthorList>
<ArticleIdList>
<ArticleId IdType="pii">JMSA2013113</ArticleId>
<ArticleId IdType="doi">10.12691/jmsa-1-1-3</ArticleId>
</ArticleIdList>
<History>
<PubDate PubStatus="received">
<Year>2013</Year>
<Month>01</Month>
<Day>14</Day>
</PubDate>
<PubDate PubStatus="revised">
<Year>2013</Year>
<Month>03</Month>
<Day>22</Day>
</PubDate>
<PubDate PubStatus="accepted">
<Year>2013</Year>
<Month>03</Month>
<Day>25</Day>
</PubDate>
</History>
<Abstract>Viscous and incompressible flow is simulated over an equilateral triangular obstacle placed in a horizontal channel. Different from the previous studies, the governing Navier-Stokes equations along with appropriate boundary conditions are solved by a particular finite volume generated code. A fixed blockage ratio (¦Â=0.05) is considered. Different ranges of Reynolds numbers in laminar regime under critical value of the Reynolds number (Re ¡Ü 38.03) are investigated. Range of this study is from 1.4 to 38.03. The flow characteristics are analyzed in the forms of streamlines and pressure fields at various Reynolds numbers. Diagram of drag coefficient versus Reynolds numbers is presented and discussed. Results are compared with the available data in the literature that display good agreements.</Abstract>
</Article>
</ArticleSet>
