Flow Parameters Behind an Unsteady Curved Shock Wave in an Ideal Gas with Heat Addition

Authors

  • B. G. Verma University of Gorakhpur, Gorakhpur

DOI:

https://doi.org/10.14429/dsj.17.7384

Keywords:

Curved Shock Wave

Abstract

This paper discusses the flows immediately behind and in front of a two dimensional unsteady curved shock wave in an ideal gas with heat addition. Method evolved by Thomas has been followed to obtain formulas for the determination of the gradients of velocity components, pressure and density behind the shock when the flow in front is known.

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Published

2014-05-21

How to Cite

Verma, B. G. (2014). Flow Parameters Behind an Unsteady Curved Shock Wave in an Ideal Gas with Heat Addition. Defence Science Journal, 17(3), 145–150. https://doi.org/10.14429/dsj.17.7384

Issue

Vol. 17 No. 3

Section

Research Papers

License

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