Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93043
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Title: Investigation on shock induced stripping breakup process of a liquid droplet
Authors: Liu, Y 
Guan, B 
Wen, CY 
Shen, H
Issue Date: 2017
Source: 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China, AIAA 2017-2369, Session: Hypersonic Fundamentals and History X
Abstract: Stripping breakup process of a single liquid droplet under the impact of a planar shock wave is investigated both experimentally and numerically. The droplet breakup experiment is conducted in a horizontal shock tube and the evolution of the droplet is recorded by direct high-speed photography. The experimental images clearly illustrate the droplet interface evolution features from its early to relatively late stage. Compressible Euler equations are solved using an in-house inviscid upwind characteristic space-time conservation element and solution element (CE/SE) method coupled with the HLLC approximate Riemann solver. A reduced five-equation model is employed to demonstrate the air/liquid interface. Numerical results accurately reproduce the water column and axi-symmetric water droplet breakup processes in experiments. The present study confirms the validity of the present numerical method in solving the shock wave induced droplet breakup problem and elaborates the stripping breakup process numerically in a long period. Droplet inner flow pattern is depicted, based on which the drives of protrusions emerged on the droplet surface are clearly seen. The droplet deformation is proved to be determined by not only the outer air flow, but also the inner liquid flow.
ISBN: 9781624104633
DOI: 10.2514/6.2017-2369
Rights: Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
The following publication Liu, Y., Wen, C., Shen, H., & Guan, B. (2017). Investigation on Shock Induced Stripping Breakup Process of A Liquid Droplet. In 21st AIAA International Space Planes and Hypersonics Technologies Conference, 6-9 March 2017, Xiamen, China, AIAA 2017-2369 is available at https://doi.org/10.2514/6.2017-2369
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