Publication | Closed Access
Experimental and Numerical Modeling of the Bow Shock Interaction with Pulse-Heated Air Bubbles
58
Citations
19
References
2010
Year
AeroacousticsEngineeringFluid MechanicsMechanical EngineeringAcoustic CavitationBubble DynamicGas DynamicNumerical SimulationMach 2Numerical ModelingShock CompressionBow Shock InteractionPhysicsMultiphase FlowPulse-heated Air BubblesSupersonic CombustionCavitating FlowAerospace EngineeringAerodynamicsBlunt BodyShock Deformation
The influence of various parameters characterizing the single- and double-pulse energy deposition (ED) upstream of a blunt body (distance between the deposition point and the body, amount of the energy and time delay between the pulses) on the topology of the supersonic flow at Mach 2 is studied experimentally and numerically. The obtained pressure-time diagram at the upstream stagnation point of the body as well as some significant topological properties of the bow-shock / heated-bubble interaction, like shock deformation and reflection, as well as the evolution of the heated bubble into the vortex ring downstream, are analyzed as resulting from the shock-decelerated spherical light-gas inhomogeneity. The evolution and topology of the interfering heated bubbles by double-pulse ED show the significance of vorticity generation initiated by blast-waves coming from the neighboring bubbles.
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