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Field of Research : Aerospace Engineering
Field of Research : Aerodynamics
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  • Funded Activity

    Linkage - International - Grant ID: LX0242362

    Funder
    Australian Research Council
    Funding Amount
    $39,856.00
    Summary
    Control of Transitions in Wakes and Swirling Flows. We will attack industrially-important problems in fluid mechanics by building new, and substantially enhancing existing, international collaborations between key complementary teams of internationally-recognised French and Australian researchers. Funding will support the exchange of 6 senior staff and 3 graduate students, which, in turn, will measurably benefit the research output of a further 20 graduate students and 7 post-doctoral fellows as .... Control of Transitions in Wakes and Swirling Flows. We will attack industrially-important problems in fluid mechanics by building new, and substantially enhancing existing, international collaborations between key complementary teams of internationally-recognised French and Australian researchers. Funding will support the exchange of 6 senior staff and 3 graduate students, which, in turn, will measurably benefit the research output of a further 20 graduate students and 7 post-doctoral fellows associated with closely-related projects. From the Australian perspective, the planned exchanges will bring new research expertise, knowledge and skills, which will be focussed on a diverse range of applications. Target industries (with existing collaborations) include Airbus and Dassault Aviation in Europe, and Aerosonde and Warman pumps in Australia.
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    Funded Activity

    Discovery Projects - Grant ID: DP0666941

    Funder
    Australian Research Council
    Funding Amount
    $350,000.00
    Summary
    Physics of Base Flows of Planetary Entry Configurations. Continued investment by Australia in the AHI will help to maintain Australia's leading role in the exciting fields of space research and hypersonics and to encourage future international collaboration. The research will use the unique existing experimental infrastructure (largely ARC funded) for space related research, which will enable Australia to make a valuable contribution to the design of future planetary missions. The project will p .... Physics of Base Flows of Planetary Entry Configurations. Continued investment by Australia in the AHI will help to maintain Australia's leading role in the exciting fields of space research and hypersonics and to encourage future international collaboration. The research will use the unique existing experimental infrastructure (largely ARC funded) for space related research, which will enable Australia to make a valuable contribution to the design of future planetary missions. The project will provide a stimulating, exciting and supportive environment for the training of postgraduate and postdoctoral personnel as well as students at the undergraduate level. It will help to motivate young Australians to pursue their interest in science and engineering.
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    Funded Activity

    Linkage Projects - Grant ID: LP0991170

    Funder
    Australian Research Council
    Funding Amount
    $350,000.00
    Summary
    The development of active third-generation heavy vehicle aerodynamic drag reducing devices to reduce future transport emissions. The potential for emission reductions through aerodynamic improvements is particularly apparent in long haul heavy vehicle transport. By developing active devices to be fitted to the heavy vehicle trailer of the future this work offers drag reduction potential from current levels of up to 40 per cent. If widely implemented these devices could play a major part in the t .... The development of active third-generation heavy vehicle aerodynamic drag reducing devices to reduce future transport emissions. The potential for emission reductions through aerodynamic improvements is particularly apparent in long haul heavy vehicle transport. By developing active devices to be fitted to the heavy vehicle trailer of the future this work offers drag reduction potential from current levels of up to 40 per cent. If widely implemented these devices could play a major part in the transport sector meeting medium term emissions targets. If successful not only will the project develop unique components, it will support heavy vehicle research and development that is so important to maintaining a strong manufacturing presence in Australia, especially in regional centres, such as Ballarat where Maxitrans has major headquarters.
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    Funded Activity

    Discovery Projects - Grant ID: DP0452374

    Funder
    Australian Research Council
    Funding Amount
    $1,805,000.00
    Summary
    Mach 10 Hydrogen fuelled scramjet development. Safe and economic access to space is a major technological challenge of the 21st century. Airbreathing engines, in particular, scramjets offer the potential to meet this challenge. The project aims to develop an understanding of the engineering and physical principals that determines the performance of a class of scramjet operating at hypervelocity speeds (>3km/s). Novel and innovative ideas will be explored which for the first time will provide .... Mach 10 Hydrogen fuelled scramjet development. Safe and economic access to space is a major technological challenge of the 21st century. Airbreathing engines, in particular, scramjets offer the potential to meet this challenge. The project aims to develop an understanding of the engineering and physical principals that determines the performance of a class of scramjet operating at hypervelocity speeds (>3km/s). Novel and innovative ideas will be explored which for the first time will provide the understandings necessary to make well founded predictions of the cost effectiveness of this approach, as well as provide the blue print to develop an engine which can operate at Mach 10.
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    Funded Activity

    Linkage Projects - Grant ID: LP0215943

    Funder
    Australian Research Council
    Funding Amount
    $146,000.00
    Summary
    Development of large scale expansion tubes. The aim of this proposal is to develop a high Mach number scramjet simulation capability by modifying the X3 superorbital expansion tube at UQ for high suborbital operation at very high total pressures. This will enable Australia to do true Mach number simulation at higher speeds than is possible anywhere else, and mantain an international advantage in the development of scramjet flight propulsion. It will also put Australian researchers in a strong p .... Development of large scale expansion tubes. The aim of this proposal is to develop a high Mach number scramjet simulation capability by modifying the X3 superorbital expansion tube at UQ for high suborbital operation at very high total pressures. This will enable Australia to do true Mach number simulation at higher speeds than is possible anywhere else, and mantain an international advantage in the development of scramjet flight propulsion. It will also put Australian researchers in a strong position to participate in the next generation of US ground testing facilities, foreshadowed by the recent NASA purchase of a large shock tunnel driver. It will enable Australia to maintain a position of leadership in the development of new space travel concepts.
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    Funded Activity

    Linkage Projects - Grant ID: LP0349258

    Funder
    Australian Research Council
    Funding Amount
    $280,000.00
    Summary
    Design and development of an innovative next generation wind driven rotating ventilator. With increasing environmental awareness, the demand for a wind-driven rotating ventilator for natural ventilation in dwellings, factories and transport vehicles is rising dramatically. This device requires no expenditure to operate or maintain and is pollution-free. However, significant safety concerns for its operation in high wind and rain remain. This project will facilitate a greater understanding of the .... Design and development of an innovative next generation wind driven rotating ventilator. With increasing environmental awareness, the demand for a wind-driven rotating ventilator for natural ventilation in dwellings, factories and transport vehicles is rising dramatically. This device requires no expenditure to operate or maintain and is pollution-free. However, significant safety concerns for its operation in high wind and rain remain. This project will facilitate a greater understanding of the complex flow phenomenon and produce innovative aerodynamic and smart solutions. The outcomes will establish Australia as the leading provider of air quality and comfort in the world, benefit particularly the rural sector and have significant positive impact on the national economy and environment.
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    Funded Activity

    Discovery Projects - Grant ID: DP0208744

    Funder
    Australian Research Council
    Funding Amount
    $284,000.00
    Summary
    Minimizing hypersonic skin-friction by boundary-layer combustion. The high drag associated with hypersonic flight has been a major obstacle to development of hypersonic aircraft. It is generally accepted that half the drag of hypersonic vehicles will be caused by air friction on the aircraft's skin, due mainly to the turbulent boundary layer which forms on the skin. However, a new method of reducing skin friction, by injecting and burning fuel in the boundary layer, has been discovered. This .... Minimizing hypersonic skin-friction by boundary-layer combustion. The high drag associated with hypersonic flight has been a major obstacle to development of hypersonic aircraft. It is generally accepted that half the drag of hypersonic vehicles will be caused by air friction on the aircraft's skin, due mainly to the turbulent boundary layer which forms on the skin. However, a new method of reducing skin friction, by injecting and burning fuel in the boundary layer, has been discovered. This project is aimed at investigating the range of conditions under which this method will be effective. By this boundary-layer "lubrication" much more efficient hypersonic flight will be possible.
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    Funded Activity

    Discovery Projects - Grant ID: DP0773371

    Funder
    Australian Research Council
    Funding Amount
    $490,000.00
    Summary
    Radiating hypersonic flows. Benefits will accrue through the involvement of Australia in the international program for future space missions. Through this project, Australia, already among the leaders in scramjet propulsion development, can also become a major player in spacecraft design. Significant educational benefits will be created due to the challenging nature of the work, through immediate contact with leading overseas researchers, and through subsequent marketing of flight vehicles. The .... Radiating hypersonic flows. Benefits will accrue through the involvement of Australia in the international program for future space missions. Through this project, Australia, already among the leaders in scramjet propulsion development, can also become a major player in spacecraft design. Significant educational benefits will be created due to the challenging nature of the work, through immediate contact with leading overseas researchers, and through subsequent marketing of flight vehicles. The project could lead to the involvement of Australian technology at a commercial level in a new generation of hardware for space exploration.
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    Funded Activity

    Linkage - International - Grant ID: LX0348303

    Funder
    Australian Research Council
    Funding Amount
    $15,536.00
    Summary
    Active and Passive Techniques of Shock Wave/Boundary Layer Interaction Control. The shock wave/ boundary layer interaction (SBLI) is a formidable problem in high-speed aerodynamics. We investigate a novel method, using piezoelectric flap actuators to control the interaction. The aim is to participate in an experimental programme on SBLI control using longitudinal slots at The University of Cambridge's Engineering Department, a leading international institution for SBLI control. Their longitudina .... Active and Passive Techniques of Shock Wave/Boundary Layer Interaction Control. The shock wave/ boundary layer interaction (SBLI) is a formidable problem in high-speed aerodynamics. We investigate a novel method, using piezoelectric flap actuators to control the interaction. The aim is to participate in an experimental programme on SBLI control using longitudinal slots at The University of Cambridge's Engineering Department, a leading international institution for SBLI control. Their longitudinal slot control is very similar to unimorph control so that this research can be used to improve the understanding of unimorph control. Furthermore, their CFD program can validate our past work and allow theoretical optimisation to create a smart flap system.
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    Funded Activity

    Discovery Projects - Grant ID: DP1094851

    Funder
    Australian Research Council
    Funding Amount
    $300,000.00
    Summary
    Computing transient inflow receptivity with application to high-lift airfoils. Applications of the research will lead to more efficient wind and gas turbines, thereby reducing greenhouse gas emissions in power generation and air transport. The project will provide high-level research training for a Research Fellow and a PhD student in an emerging area that links fundamental fluid mechanics, optimal control and optimal engineering design. Also the project will foster international collaboration w .... Computing transient inflow receptivity with application to high-lift airfoils. Applications of the research will lead to more efficient wind and gas turbines, thereby reducing greenhouse gas emissions in power generation and air transport. The project will provide high-level research training for a Research Fellow and a PhD student in an emerging area that links fundamental fluid mechanics, optimal control and optimal engineering design. Also the project will foster international collaboration with partner researchers and organizations in the United Kingdom.
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