Blast wave induced unsteady flow at the shock tube opening
Saini Jatin Rao, Akhil Aravind, Saptarshi Basu

TL;DR
This study investigates the complex unsteady flow phenomena generated by blast waves in an open-ended shock tube, revealing new transient features and providing an approximate model for blast evolution and flow interactions.
Contribution
The paper introduces detailed experimental observations and an approximate model of blast wave dynamics at the shock tube opening, including previously unreported unsteady features.
Findings
Identification of reverse shock formation and embedded shock shedding.
Development of an approximate power-law density profile model.
Validation of steady-pressure outlet conditions for accurate flow prediction.
Abstract
Shock tubes have been a crucial device, facilitating studies across a wide range of practical applications. An open-ended shock tube employing the wire-explosion technique with a rectangular cross section is used in the present study to generate blast waves over a Mach number range of 1.2-1.8, enabling detailed investigation of unsteady compressible flow at the tube opening. The blast wave produces a complex flow field comprising a compressible vortex ring with a trailing jet, and several transient structures, including embedded shocks, inward-moving shock or reverse shocks, shear layers, and Prandtl-Meyer expansion fans. An approximate model based on a power-law density profile describes the blast evolution inside and outside the tube, with the equivalent source deduced from measured shock trajectories. The blast wave-tube exit interaction is analyzed using the method of…
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Taxonomy
TopicsComputational Fluid Dynamics and Aerodynamics · Laser-Plasma Interactions and Diagnostics · Combustion and Detonation Processes
