Research

Current research projects

 

Project #1: Quantitative local measurements in isotropic compressible turbulence

 


The Variable Density and Viscosity Vessel (VDSSV) is a pressure vessel about one meter in diameter. It is a laboratory in which the atmosphere can be changed – different gases such as air or sulfur hexafluoride can be maintained at pressures between 0.01 and 15 bar. Experiments in this laboratory quantify the effects of widely variable densities, viscosities and speeds of sound on fluid mechanics and turbulence.
Inside the VDSSV, a fan generates a Mach 0.7 turbulent jet in sulfur hexafluoride (SF6). The surrounding loudspeakers modulate the balance between solenoidal and dilatational motions in the turbulence. For more details, please see my recent publication in Experiments in Fluids.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Project #2: Three-dimensional mixing layer with an adjustable crossflow component

 

The Variable Density and Speed of Sound Vessel (VDSSV) is a pressure vessel about one meter in diameter. It is a laboratory in which the atmosphere can be changed – different gases such as air or sulfur hexafluoride can be maintained at pressures between 0.01 and 15 bar. Experiments in this laboratory quantify the effects of widely variable densities, viscosities and speeds of sound on fluid mechanics and turbulence.
The active grid generates homogenous turbulence. Combined with a splitter and other flow modifiers, it produces a mixing layer with adjustable lateral velocity. Credits: Peter McGurk & team

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Past research projects

 

Project #3: Nanofabrication of turbulence sensors

 

To resolve the increasingly smaller physical scales that arise with increasing flow speed, nanometers-thick, streamlined probes were nanofabricated at CNF using semiconductor manufacturing techniques. The design is inspired by Hultmark et al. (2011). Credits: Edmund Liu

 

Project #4: Bird flight dynamics captured in a field experiment

 

The flight dynamics of a red-tail hawk were analyzed from data collected in a field experiment. Rear-view and side-view trajectories were captured by cameras, whereas turbulence and wind data were collected using a sonic anemometer and a Pitot tube.