Computational Study of Viscous Flow in a Scramjet

Authors

  • Jeevan Rao Dept. of Aeronautical Engineering, Vardhaman College of Engineering, Hyderabad Author
  • Bhargav A Dept. of Aeronautical Engineering, Vardhaman College of Engineering, Hyderabad Author
  • Krupakar Pasala Dept. of Aeronautical Engineering, Vardhaman College of Engineering, Hyderabad Author
  • Srinivasa Rao Dept. of Aeronautical Engineering, Vardhaman College of Engineering, Hyderabad Author

Keywords:

Scramjet, Fuel-off, CFD etc

Abstract

The present work describes the study on complex internal viscous flow in a scramjet. The dissociation of air in complex scramjet model using two dimensional computational fluid dynamics and also at fuel-off conditions on combustion chamber is presented. The results of free-stream flow atto Mach 4 at different altitudes viz 25km, 30km and 35km in the combustion chamber are compared. For computational aid Green Gauss cell based gradient option is used with steady time and absolute velocity formulation.

References

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Published

2014-02-28

Issue

Special Issue-2 (Feb 2014)

Section

Articles

How to Cite

Computational Study of Viscous Flow in a Scramjet. (2014). International Journal of Current Engineering and Technology, 1(2.Special Issue), 480-484. https://ijcet.evegenis.org/index.php/ijcet/article/view/3690