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

  • 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.
Published
2014-05-21
How to Cite
Verma, B. (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
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