Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F13%3A00394420" target="_blank" >RIV/61388998:_____/13:00394420 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21220/13:00226694
Result on the web
<a href="http://dx.doi.org/10.1007/978-3-642-33134-3" target="_blank" >http://dx.doi.org/10.1007/978-3-642-33134-3</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1007/978-3-642-33134-3" target="_blank" >10.1007/978-3-642-33134-3</a>

Result language
angličtina
Original language name
Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers
Original language description
This study deals with the numerical solution of a 2D unsteady flow of a compressible viscous fluid in a channel for low inlet airflow velocity. The unsteadiness is caused by a prescribed periodic motion of the channel wall. Instudy three different governing systems of equations are considered ? Full system, Adiabatic system, Iso-energetic system. Unsteady flow fields for inlet Mach number M = 0.012 and frequency 100Hz are presented.
Czech name
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Czech description
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Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Numerical Mathematics and Advanced Applications 2011
ISBN
978-3-642-33133-6
ISSN
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e-ISSN
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Number of pages
9
Pages from-to
569-577
Publisher name
Springer
Place of publication
Berlin
Event location
Leicester
Event date
Sep 5, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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