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Nozzle Geometry Effects in the Near Field of a Round Jet

  • Fabrizio Tessicini
  • Roberto Verzicco
  • Paolo Orlandi
Part of the International Centre for Mechanical Sciences book series (CISM, volume 439)

Abstract

Axisymmetric numerical experiments of round jets are reported with the aim of showing the nozzle geometry effects on the jet evolution. It is shown in particular that, although the simulation of the nozzle flow has a non-negligible computational cost, its effect on the jet evolution can be very important. It is also demonstrated that the flow configuration resulting at the nozzle exhaust can not be assigned at the boundary of a computational domain without considering also the flow inside the nozzle since it is a combination of radial and axial velocity components supported by an appropriate pressure distribution.

Keywords

Shear Layer Radial Velocity Axial Velocity Centerline Velocity Nozzle Flow 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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Copyright information

© Springer-Verlag Wien 2003

Authors and Affiliations

  • Fabrizio Tessicini
    • 1
  • Roberto Verzicco
    • 2
  • Paolo Orlandi
    • 1
  1. 1.DMA, Università di Roma ‘La Sapienza’RomaItalia
  2. 2.DIMeG, Politecnico di BariBariItalia

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