The facilities utilised for aerodynamics research can broadly be broken down into two categories; computational hardware for simulation and modelling work and experimental equipment for physical testing.
Much of the work carried out by the computational researchers within the group requires significant computational power, which is obtained from Multi-CPU clusters. Multi-CPU clusters allow 'parallel' codes to be run, i.e. large problems split and run over several CPUs simultaneously, but also allow scalar codes to be run with multiple data sets simultaneously, i.e. a 'scalar farm'. The group uses two main computational resources:
This consists of a very quiet closed-circuit wind tunnel and a large anechoic chamber. The Wind tunnel is powered by a 50kW centrifugal fan and is equipped with a series of large silencers to reduce the fan noise in the ductwork. The wind tunnel is equipped with a 40kW water cooled chiller, enabling continuous testing at a set temperature, between 18o to 25 o. The anechoic chamber is approximately 7m x 4.5m x 3.5m and is fully anechoic down to 250Hz. Several contraction nozzles, with different aspect- and contraction-ratios have been made for measurement of noise from different aero-components, such as aerofoils, bluff bodies, boundary layer, etc. The working section of the wind tunnel is equipped with Dantec hotwire CTA system, 2D PIV, source location microphone array (48 microphones) and an array of GRAS and B&K free-field microphones. Two National Instrument DAQ are used in the aeroacoustics facility, enabling simultaneous data collection of up to 84 channels. The facility can also be turned into a jet noise facility with flight stream. The jet noise apparatus is connected to the main pressurized air system, with air supply of 460 lit/sec at 7bar. The jet noise measurement can be carried out in the presence of flight stream by changing the contraction nozzle to a circular nozzle. Tests can be done for jet flows of up to Mach 0.9 and with flight-stream of 120 knots (61 m/s).
Additionally the itself group holds a variety of equipment such as the EMEGG used for rocket nozzle testing.
The Hele-Shaw laboratory is a new facility specialising in different areas of fluid mechanics teaching and research. It houses the University's capability in low viscosity liquids and multi-phase interactions between liquid and gas. The space is open-plan to jointly serve the needs of teaching and research across the Faculty.
More information: bristol.ac.uk/heleshawlab