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Fluid Mixing at Extreme Conditions Laboratory

FMECL

Texas A&M University College of Engineering

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Our laboratory is interested in fluid mixing at high temperatures, pressures, and velocities. We are also interested in additional physics in these problems such as multiphase flows, and magnetohydrodynamic forces. These types of problems arise in hypersonic propulsion, detonation engines, inertial confinement fusion, astrophysics, and refrigeration technologies. We use both simulations and experiments to perform our research. Our laboratory operates a shock tube facility and we are constructing a liquid-fueled detonation tube. We use high-speed laser based diagnostics (e.g. PIV, PDPA, high-speed imaging) to measure fluid conditions in these experiments. On the simulation side of our research, we develop models for implementation in hydrodynamics codes and run simulation of shock-driven multiphase and magnetohydrodynamic problems. We use both in-house codes and codes maintained by DoE/NNSA and DoD laboratories.

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  • Shock-Driven Multiphase Instability, Particle-laden Richtmyer-Meshkov Instability
    This image shows the development of a cylindrical particle laden interface subjected to a Mach 1.35 shock wave. Each interface has the same particle mass (effective density) but different particle sizes. The images are taken at the same time but show different development due to the particle size. The image on the right has very small particles in a heavy gas (same effective density as other interface) and shows development much like a Richtmyer-Meshkov instability. As particle size increases, the circulation (mixing energy) decreases due to particle lagging behind the gas.
  • velocity, vapor concentration, and vorticity for a Richtmyer-Meshkov instability with evaporation
    These images show the development of a Shock-Driven Multiphase Instability or Richtymer-Meshkov Instability. A cylindrical intervace containing acetone droplet and vapor was accelerated by a Mach 1.67 shock wave. The droplets breakup, evaporate, and lag behind the gas flow, reducing vorticity but increasing acetone vapor concentration. Vapor concentration is visible from the magenta color in the center image, while Mie-scattered light from the droplets is visible as green.
  • 20um detonation
    Droplet breakup in a liquid fueled detonation. The detonation is traveling from right to left. Upstream droplet are visible as small points on the left. On the right, clouds of child droplets are visible as much large white regions. The child droplet clouds decay in intensity as they fall behind the shock front and are burned (moving to the right). The shock is visible as semi vertical line separating the small upstream droplets from the large child droplet clouds.
  • Gaseous Air and Decane Detonation Simulations
    These simulations are for gaseous air and decane at an equivalence ratio of one and atmospheric conditions. Images show a complex wave structure with pockets of unburned fuel falling behind the detonation front.
  • Shows the evolution of a 3D spherical SDMI
    Simulation of a shock-accelerated spherical region of 2um water droplets. Points show the sizes of droplets, and contours show the vapor fraction.
  • SDMI in experiments and simulations
    Top: The droplet field evolution over time. Bottom: Simulations of the droplet field using a droplet breakup model.

 

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