Shock Waves

, Volume 28, Issue 2, pp 335–348 | Cite as

Two-dimensional computational modeling of high-speed transient flow in gun tunnel

  • A. M. Mohsen
  • M. Z. Yusoff
  • H. Hasini
  • A. Al-Falahi
Original Article

Abstract

In this work, an axisymmetric numerical model was developed to investigate the transient flow inside a 7-meter-long free piston gun tunnel. The numerical solution of the gun tunnel was carried out using the commercial solver Fluent. The governing equations of mass, momentum, and energy were discretized using the finite volume method. The dynamic zone of the piston was modeled as a rigid body, and its motion was coupled with the hydrodynamic forces from the flow solution based on the six-degree-of-freedom solver. A comparison of the numerical data with the theoretical calculations and experimental measurements of a ground-based gun tunnel facility showed good agreement. The effects of parameters such as working gases and initial pressure ratio on the test conditions in the facility were examined. The pressure ratio ranged from 10 to 50, and gas combinations of air–air, helium–air, air–nitrogen, and air–\(\hbox {CO}_{2}\) were used. The results showed that steady nozzle reservoir conditions can be maintained for a longer duration when the initial conditions across the diaphragm are adjusted. It was also found that the gas combination of helium–air yielded the highest shock wave strength and speed, but a longer test time was achieved in the test section when using the \(\hbox {CO}_{2}\) test gas.

Keywords

Gun tunnel Shock wave Mach number CFD 

Notes

Acknowledgements

The authors would like to sincerely thank the Ministry of Higher Education (MOHE) of Malaysia for the provision of a Grant with code No. 20150213FRGS to support this work.

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Copyright information

© Springer-Verlag GmbH Germany 2017

Authors and Affiliations

  • A. M. Mohsen
    • 1
  • M. Z. Yusoff
    • 1
  • H. Hasini
    • 1
  • A. Al-Falahi
    • 2
  1. 1.Centre for Advanced Computational Engineering, College of EngineeringUniversiti Tenaga NasionalKajangMalaysia
  2. 2.Sheridan CollegeBramptonCanada

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