Abstract. A two-dimensional theory is developed for the vorticity just downstream of a curved, unsteady shock wave. By utilizing Crocco's equation, an explicit formula is obtained for the vorticity that does not require a perfect gas and that holds for arbitrary conditions upstream of the shock wave. The analysis is applied to the flow just downstream of the reflected shock that occurs in a single-Mach reflection pattern. Flow conditions are based on an interferometric photograph of Ben-Dor and Glass (1978). In this case, the reflected shock is weak everywhere from its upstream intersection with the wall to the triple point. The vorticity has a singularity and a change of sign near the triple point that indicates the presence of a weak shear layer downstream of this location.
Similar content being viewed by others
Author information
Authors and Affiliations
Additional information
Received 20 December 1999 / Accepted 19 March 2000
Rights and permissions
About this article
Cite this article
Yi, T., Emanuel, G. Unsteady shock generated vorticity. Shock Waves 10, 179–184 (2000). https://doi.org/10.1007/s001930050004
Issue Date:
DOI: https://doi.org/10.1007/s001930050004