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Research Topic : Aerospace structures
Socio-Economic Objective : Space transport
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Aerospace Engineering (10)
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  • Funded Activity

    Discovery Projects - Grant ID: DP0666683

    Funder
    Australian Research Council
    Funding Amount
    $275,000.00
    Summary
    Shape adaptive structures with built-in compact smart material based actuators. Primary Australian aerospace manufacturers are sub-contractors and constantly compete in the global market. Their products are primarily control surfaces, e.g., Boeing 757 and 777 rudders, 737 Krueger flaps. In light of the development of the hingeless control surfaces (HCS) in the smart aircraft wing program in the USA, the economic benefits of this project are very high because (a) it will address the key technolo .... Shape adaptive structures with built-in compact smart material based actuators. Primary Australian aerospace manufacturers are sub-contractors and constantly compete in the global market. Their products are primarily control surfaces, e.g., Boeing 757 and 777 rudders, 737 Krueger flaps. In light of the development of the hingeless control surfaces (HCS) in the smart aircraft wing program in the USA, the economic benefits of this project are very high because (a) it will address the key technological issue identified in the HCS program; and (b) it will enhance Australian manufacturers¡¯ technological standing and input in the design and manufacturing of next generation HCS by providing highly trained people with world-leading niche technology.
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    Funded Activity

    Discovery Projects - Grant ID: DP0210716

    Funder
    Australian Research Council
    Funding Amount
    $279,000.00
    Summary
    Active shape control of large thin-walled structures using ferroelectric single crystals. Ferroelectric single crystals were invented 5 years ago, and they possess many superior properties compared to conventional piezoelectric materials, particularly the induced strain up to 1.5%, an order higher than conventional materials. This project aims to poineer the application of these new and powerful smart materials as actuators and sensors to shape control of smart structures. The expected outcome .... Active shape control of large thin-walled structures using ferroelectric single crystals. Ferroelectric single crystals were invented 5 years ago, and they possess many superior properties compared to conventional piezoelectric materials, particularly the induced strain up to 1.5%, an order higher than conventional materials. This project aims to poineer the application of these new and powerful smart materials as actuators and sensors to shape control of smart structures. The expected outcomes are (a) a new constitutive theory for the non-linear behaviour of ferroelectric single crystals; (b) a novel definition and formulation for the shape control problem; and (c) an innovative theoretical framework for design optimization of shape control of smart structures using ferroelectric single crystals.
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    Funded Activity

    Discovery Projects - Grant ID: DP0774596

    Funder
    Australian Research Council
    Funding Amount
    $351,942.00
    Summary
    Morphing flexible structures with lead lanthanum zirconium titanate (PLZT) based optical actuators. Lead lanthanum zirconate titanate (PLZT) materials yield mechanical strains when exposed to near ultraviolet light as a result of combined photovoltaic and converse piezoelectric effects. They offer actuation strain on par with piezoelectric materials and other advantages, such as wireless light-to-mechanical energy transfer, immunity from electrical and magnetic disturbances and fast response wi .... Morphing flexible structures with lead lanthanum zirconium titanate (PLZT) based optical actuators. Lead lanthanum zirconate titanate (PLZT) materials yield mechanical strains when exposed to near ultraviolet light as a result of combined photovoltaic and converse piezoelectric effects. They offer actuation strain on par with piezoelectric materials and other advantages, such as wireless light-to-mechanical energy transfer, immunity from electrical and magnetic disturbances and fast response with the transparent electrode design. This project aims to pioneer the application of PLZT optical actuators in morphing flexible structures leading to development of wireless smart structures technology and opt-electromechanical systems such as medical instruments.
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    Funded Activity

    Discovery Projects - Grant ID: DP0346419

    Funder
    Australian Research Council
    Funding Amount
    $162,000.00
    Summary
    Controlled vibration of intelligent super-lightweight structure systems. This project aims to poineer research on dynamic shape control of intelligent structure systems, in which the rapid shape variation of a structure is controlled with fast varying electric energy. It bridges the gap between structural shape and vibration control. The expected outcomes are (a) novel concepts and formulation of dynamic shape control; (b) biologically inspired active stiffener system; and (c) an innovative th .... Controlled vibration of intelligent super-lightweight structure systems. This project aims to poineer research on dynamic shape control of intelligent structure systems, in which the rapid shape variation of a structure is controlled with fast varying electric energy. It bridges the gap between structural shape and vibration control. The expected outcomes are (a) novel concepts and formulation of dynamic shape control; (b) biologically inspired active stiffener system; and (c) an innovative theoretical framework for design optimization of dynamic shape control of intelligent structure systems.
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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

    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

    Discovery Projects - Grant ID: DP1094560

    Funder
    Australian Research Council
    Funding Amount
    $490,000.00
    Summary
    Hypervelocity re-entry. Addressing a critical area of space travel and its practical utilisation it will help expand a key technology niche which will facilitate our involvement in major programs of the future. In international space programs each participant provides a unique technical contribution and shares in the intellectual and economic returns. Educational benefits arise due to the challenging nature of the work, contact with overseas researchers, and through the marketing and developm .... Hypervelocity re-entry. Addressing a critical area of space travel and its practical utilisation it will help expand a key technology niche which will facilitate our involvement in major programs of the future. In international space programs each participant provides a unique technical contribution and shares in the intellectual and economic returns. Educational benefits arise due to the challenging nature of the work, contact with overseas researchers, and through the marketing and development of flight vehicles and associated technology. There will be opportunity for our graduates to be employed in senior positions overseas, and to subsequently return to Australia with advanced skills and facilitate Australian collaboration from positions of influence.
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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

    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: DP0665016

    Funder
    Australian Research Council
    Funding Amount
    $260,000.00
    Summary
    Enhancing scramjet performance by boundary layer combustion. Australia has developed a strong international reputation over the past 20 years for excellence in research into hypersonic flight technologies. This helps to reinforce the fact that this is a country in which advanced technologies can be conceived and developed. Australian companies and agencies are already collaborating with and are being supported by international organizations to develop further hypersonic flight technologies. Achi .... Enhancing scramjet performance by boundary layer combustion. Australia has developed a strong international reputation over the past 20 years for excellence in research into hypersonic flight technologies. This helps to reinforce the fact that this is a country in which advanced technologies can be conceived and developed. Australian companies and agencies are already collaborating with and are being supported by international organizations to develop further hypersonic flight technologies. Achieving another significant advance in this area by demonstrating significant reductions in frictional drag on hypersonic vehicles will keep us at the forefront of this field and lead to continued international support and collaboration.
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