Flow field and acoustic characteristics of compressible vortex ring
evolution and its interaction with wall have been investigated for
Mach number varying from 1.3 to 1.85 using high speed smoke
visualizations and microphone. Importance of vortex ring study,
classifications, generation mechanism, parameters that characterize
its evolution and time line of vortex rings research since its
discovery are discussed in Chap. 1. Shock tube design and theory of
shock tube flow with the history and applications of shock tube are
discussed in Chap. 2 and appendix A. The spatial and angular
variations of incident shock diffracted at the shock tube exit are
also studied using hot wire anemometer. The effect of driver
section length, its pressure, and various driver section gases on
shock strength and uniform flow time is discussed using method of
characteristics (MOC) technique. Evolution of primary and counter
rotating vortex rings (CRVR) are studied in chap. 3 and 4. Vortex
ring diameter increases rapidly and translational velocity
decreases during the formation and evolution of CRVR. The shock and
wall interaction of vortex ring are discussed in Chap. 5.
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