Numerical Investigation of Liquid Droplet Interactions with Cylindrical Bow Shocks
ORAL
Abstract
Precipitation and suspended droplets in the atmosphere present a significant erosion risk to vehicles traveling and high-supersonic and hypersonic speeds. We will present the results of simulations considering the interactions of droplets with blunt projectiles in a high-supersonic (Mach 2-4) flow environment. We use a volume of fluid method implemented in the compressibleInterFoam solver of OpenFOAM to simulate the interaction of a water droplet with the bow shock generated by a cylindrical blunt body. The droplet size, droplet position, blunt body diameter, and flow mach number are varied to determine the regimes where direct impact, partial impact, or no impact occurs as governed by the degree of droplet breakup driven by aerodynamic forces in the shock layer.
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Presenters
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Andrew M Hess
United States Naval Research Laboratory
Authors
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Andrew M Hess
United States Naval Research Laboratory
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David A Kessler
United States Naval Research Laboratory, Naval Research Laboratory
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Ryan F Johnson
United States Naval Research Laboratory