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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.
  • 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. (en)
Title
  • Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers
  • Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers (en)
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  • Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers
  • Numerical comparison of unsteady channel compressible flow with low inlet Mach numbers (en)
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  • RIV/61388998:_____/13:00394420!RIV14-GA0-61388998
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  • I, P(GAP101/11/0207)
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  • 92531
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  • RIV/61388998:_____/13:00394420
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  • vocal tract; mathematical model; finite volume method; adiabatic and Iso-energetic systems (en)
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  • [1BE058357D3D]
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  • Leicester
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  • Berlin
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  • Numerical Mathematics and Advanced Applications 2011
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  • Horáček, Jaromír
  • Kozel, Karel
  • Pořízková, P.
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number of pages
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  • 10.1007/978-3-642-33134-3
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  • Springer-Verlag
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  • 978-3-642-33133-6
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