Linkage Infrastructure, Equipment And Facilities - Grant ID: LE170100203
Funder
Australian Research Council
Funding Amount
$326,000.00
Summary
Flow measurement for large-scale industrial aerodynamics. This project aims to research the unsteady aerodynamic wakes of cars, trucks, athletes, turbines and micro-air vehicles. Researchers will use the flow measurement system for large-scale industrial aerodynamics to resolve high speed and large scale industrial flows. The system’s primary objective will be the characterisation of complex, three-dimensional turbulent flows. It is anticipated that the research will lead to reduced aerodynamic ....Flow measurement for large-scale industrial aerodynamics. This project aims to research the unsteady aerodynamic wakes of cars, trucks, athletes, turbines and micro-air vehicles. Researchers will use the flow measurement system for large-scale industrial aerodynamics to resolve high speed and large scale industrial flows. The system’s primary objective will be the characterisation of complex, three-dimensional turbulent flows. It is anticipated that the research will lead to reduced aerodynamic drag in transport and improve wind power generation, ultimately reducing emissions and improving efficiency and national competitiveness in sport. The advanced system will strengthen Australia’s position as an advanced engineering design hub.Read moreRead less
Turbulent wall-bounded flow in adverse pressure gradient environments. This research will create additional research capacity in turbulence control and drag reduction. It will have direct benefits to the Australian economy via the transport industry by reducing the adverse impact of the carbon tax and rising fuel prices on long-haul air, water and road transport, on which Australia is disproportionately reliant.
Lower greenhouse at lower cost: maximising the potential of liquefied petroleum gas (LPG) in passenger vehicles. This project will develop tools for designing internal combustion engines that simultaneously achieve low greenhouse emissions without added consumer cost. The project aim is to be achieved through the effective use of liquefied petroleum gas (LPG), which is an affordable fuel that has potentially low emissions if used properly.
Advanced Combustion Modelling for Scramjets and Rotating Detonation Engines. This project will develop new fundamental knowledge and engineering models underpinning air-breathing high speed propulsion engines employing complex hydrocarbon fuels. Extensive data and new physical understanding will be garnered through analysis of direct numerical simulations of supersonic reacting mixing layers including impinging shock waves. That data will be employed to isolate, test and develop computationally ....Advanced Combustion Modelling for Scramjets and Rotating Detonation Engines. This project will develop new fundamental knowledge and engineering models underpinning air-breathing high speed propulsion engines employing complex hydrocarbon fuels. Extensive data and new physical understanding will be garnered through analysis of direct numerical simulations of supersonic reacting mixing layers including impinging shock waves. That data will be employed to isolate, test and develop computationally efficient engineering models that are accurate and efficient for high speed combustion in rotating detonation engines and scramjets. Expected outcomes are knowledge and tools needed to develop practical and effective supersonic propulsion engines for access to space, defence and high speed point-to-point flight.
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Linkage Infrastructure, Equipment And Facilities - Grant ID: LE200100042
Funder
Australian Research Council
Funding Amount
$340,000.00
Summary
Next generation facility to measure microfluidic flows. Microfluidics is ubiquitous in society - for example, biofluids and engineered lab-on-a-chip platforms. This project aims to establish a novel flow measurement facility tailored for microfluidic flows with capabilities beyond current commercial flow diagnostic systems. This will enable engineers and scientists to probe the fluid dynamics of these flows with unprecedented detail to explain their underlying physical mechanisms. Beyond fluidic ....Next generation facility to measure microfluidic flows. Microfluidics is ubiquitous in society - for example, biofluids and engineered lab-on-a-chip platforms. This project aims to establish a novel flow measurement facility tailored for microfluidic flows with capabilities beyond current commercial flow diagnostic systems. This will enable engineers and scientists to probe the fluid dynamics of these flows with unprecedented detail to explain their underlying physical mechanisms. Beyond fluidic measurement, the facility provides the capacity to accurately observe micro-organisms, biological activity (cell adhesion, thrombus stability, fluorescent receptor markers), thermal collector systems (high flux, microchannel-based solar receivers), and many more mechanical phenomena at the micro-scale.
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Turbulent flow over surfaces with spatially varying roughness. This project aims to improve understanding of the effect of spatial roughness transitions on turbulent flows. Fluids flowing over non-smooth surfaces influence our daily lives, such as water moving through a pipe, wind blowing over the Earth's surface or aircraft moving through air. The presence of surface roughness profoundly influences these flows. Though engineers have learnt to deal effectively with evenly distributed roughness, ....Turbulent flow over surfaces with spatially varying roughness. This project aims to improve understanding of the effect of spatial roughness transitions on turbulent flows. Fluids flowing over non-smooth surfaces influence our daily lives, such as water moving through a pipe, wind blowing over the Earth's surface or aircraft moving through air. The presence of surface roughness profoundly influences these flows. Though engineers have learnt to deal effectively with evenly distributed roughness, this is seldom encountered in reality. Rather, there are abrupt changes in roughness, for example at the edges of wind-farms or at rivets on aircraft. This project aims to investigate these important, but little understood, turbulent flows. Potential benefits include improved simulation, more efficient vehicle design and improved atmospheric and climate models.Read moreRead less
Silencing the screech tone - noise suppression in supersonic jets. The focus of this research is to further develop understanding of the fundamental mechanics of the aeroacoustic phenomenon known as screech. From this deeper understanding a range of tailored control mechanisms are expected to be developed to reduce or eliminate the effects of screech in the engines of high-speed aircraft. The research builds on existing expertise and established experimental facilities. As well as an improved un ....Silencing the screech tone - noise suppression in supersonic jets. The focus of this research is to further develop understanding of the fundamental mechanics of the aeroacoustic phenomenon known as screech. From this deeper understanding a range of tailored control mechanisms are expected to be developed to reduce or eliminate the effects of screech in the engines of high-speed aircraft. The research builds on existing expertise and established experimental facilities. As well as an improved understanding of fundamental mechanism, the expected outcomes of the research are more efficient active and passive flow control devices for the reduction of supersonic jet noise.Read moreRead less
Elliptical nozzles: the shape of silence? This project aims to leverage the aeroacoustic properties of elliptical nozzle geometries to significantly reduce installed jet noise. This project expects to generate new knowledge regarding methods to reduce installed jet noise, a serious problem for the aerospace industry. Regulatory constraints inhibit the implementation of efficiency-increasing configurations but still fail to eliminate public health impacts. Expected outcomes include a set of tools ....Elliptical nozzles: the shape of silence? This project aims to leverage the aeroacoustic properties of elliptical nozzle geometries to significantly reduce installed jet noise. This project expects to generate new knowledge regarding methods to reduce installed jet noise, a serious problem for the aerospace industry. Regulatory constraints inhibit the implementation of efficiency-increasing configurations but still fail to eliminate public health impacts. Expected outcomes include a set of tools for optimizing nozzle designs capable of significantly reducing installed jet noise. This will provide significant benefits, as jet noise is a serious health issue for the Australian public. This project represents an opportunity to reduce its impact while improving fuel efficiency.Read moreRead less
The underexpanded impinging jet: a self-forcing flow of critical importance. The project aims to support the development and optimisation of a wide range of industrial processing techniques based on an in-depth understanding of receptivity mechanisms in the under-expanded impinging jet flow. Under-expanded impinging jets have broad applications ranging from aerospace propulsion to additive manufacturing to pharmaceutical drug delivery. By elucidating the underlying physics of this highly complex ....The underexpanded impinging jet: a self-forcing flow of critical importance. The project aims to support the development and optimisation of a wide range of industrial processing techniques based on an in-depth understanding of receptivity mechanisms in the under-expanded impinging jet flow. Under-expanded impinging jets have broad applications ranging from aerospace propulsion to additive manufacturing to pharmaceutical drug delivery. By elucidating the underlying physics of this highly complex flow field, the project aims to facilitate active control methodologies in a range of key industrial flows. The expected outcomes of the research include improving the efficiency and efficacy of a number of industrial processes, as well as increased knowledge about the fundamental science.Read moreRead less
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE110100079
Funder
Australian Research Council
Funding Amount
$500,000.00
Summary
Experimental facility for extreme air/sea interaction studies. The level of greenhouse gases in the atmosphere which cause global warming is greatly influenced by interactions at the air/sea interface. This infrastructure will allow in-depth studies of these interactions and contribute to much improved strategies to control greenhouse gases.