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Interaction of a Supersonic Underexpanded Jet with a Flat Plate

  • O. AmiliEmail author
  • D. Edgington-Mitchell
  • D. Honnery
  • J. Soria
Conference paper
Part of the Lecture Notes in Mechanical Engineering book series (LNME)

Abstract

High-spatial resolution measurements of the velocity field of a supersonic jet impinging on a flat surface were conducted. To study the effect of the boundary condition, two nozzle outer geometries were investigated. The experimental results presented here are for a nozzle pressure ratio of NPR = 3.0 and a nozzle to plate spacing of \(Z/D = 3.5\). The flow fields of the corresponding cases show that although the general features of the flow are similar, the ambient air entrainment into the shear layer is different. This change in entrainment influences the rest of the jet structure.

Keywords

Particle Image Velocimetry Shear Layer Digital Particle Image Velocimetry Nozzle Pressure Ratio Shock Cell 
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.

Notes

Acknowledgments

The financial support to conduct this research by the Australian Research Council is gratefully acknowledged. This research was undertaken with the assistance of resources from the National Computational Infrastructure (NCI), which is supported by the Australian Government.

References

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Copyright information

© Springer-Verlag Berlin Heidelberg 2016

Authors and Affiliations

  • O. Amili
    • 1
    Email author
  • D. Edgington-Mitchell
    • 1
  • D. Honnery
    • 1
  • J. Soria
    • 1
    • 2
  1. 1.Laboratory for Turbulence Research in Aerospace and Combustion, Department of Mechanical and Aerospace EngineeringMonash UniversityMelbourneAustralia
  2. 2.Department of Aeronautical EngineeringKing Abdulaziz UniversityJeddahKingdom of Saudi Arabia

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