Aerothermodynamics and Fluid Mechanics

woman in lab with large flame

This area involves study and research in hypersonics, aerodynamics, gas dynamics, turbulence, plasma dynamics, heat transfer, and combustion.

Research is presently being conducted in nonequilibrium and rarefied gas flows, turbulence control, shock-boundary layer interactions, thermal and glow-discharge plasmas, turbulent mixing/combustion, nonlinear flow interactions, and advanced optical diagnostics and sensors. Facilities include Mach 2 and Mach 5 blowdown wind tunnels, a 1.25-second low-gravity drop tower, 15" by 20" water channel, laser sensor laboratory, combustion facilities, plasma engineering laboratory, an anechoic chamber facility for rocket nozzle testing, and extensive laser and camera systems for advanced flow diagnostics. The excellent TACC computational facilities include a variety of workstations and access to high-performance computers.

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