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Aerospace engineering / Drag / Shock wave / Mach number / Compressible flow / Bow shock / Reynolds number / Wake / Aerodynamics / Fluid mechanics / Fluid dynamics
Date: 2014-04-08 12:03:27
Aerospace engineering
Drag
Shock wave
Mach number
Compressible flow
Bow shock
Reynolds number
Wake
Aerodynamics
Fluid mechanics
Fluid dynamics

The Effects of Shock Strength on Droplet Breakup Jomela C. Meng and Tim Colonius 1 Introduction The breakup of droplets occurs in the combustion of multiphase mixtures and the

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