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Scheme : Linkage Projects
Research Topic : Aerodynamics
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  • Researchers (22)
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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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    Active Funded Activity

    Linkage Projects - Grant ID: LP210301072

    Funder
    Australian Research Council
    Funding Amount
    $1,009,570.00
    Summary
    Remote diagnostics for space-access flight testing. Aerospace flight testing is essential for assessing the reliability of space-access technologies including re-usable rockets and hypersonic air-breathing systems. Development of such technologies relies on acquisition of optical data in video and scientific formats, and such capabilities are now required in Australia. By leveraging contributions to international missions, this project develops the essential optical diagnostic tools and techniqu .... Remote diagnostics for space-access flight testing. Aerospace flight testing is essential for assessing the reliability of space-access technologies including re-usable rockets and hypersonic air-breathing systems. Development of such technologies relies on acquisition of optical data in video and scientific formats, and such capabilities are now required in Australia. By leveraging contributions to international missions, this project develops the essential optical diagnostic tools and techniques and establishes an enduring capability for space-access flight testing in Australia, thereby accelerating the research and development pathways for Australian enterprises and designating Australia as a prime destination for international aerospace businesses.
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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

    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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    Active Funded Activity

    Linkage Projects - Grant ID: LP180100107

    Funder
    Australian Research Council
    Funding Amount
    $475,000.00
    Summary
    Electron Transpiration Cooling of Hypersonic Vehicles. Future aircraft for flight at hypersonic speeds require sharp leading edges for the best aerodynamic performance. Sharp leading edges incur high heat loads and cannot be adequately cooled with current technologies. The project aim is to investigate novel surface materials that emit electrons when heated. This emission of electrons from the surface can significantly contribute to the cooling of the sharp leading edges. This project is expecte .... Electron Transpiration Cooling of Hypersonic Vehicles. Future aircraft for flight at hypersonic speeds require sharp leading edges for the best aerodynamic performance. Sharp leading edges incur high heat loads and cannot be adequately cooled with current technologies. The project aim is to investigate novel surface materials that emit electrons when heated. This emission of electrons from the surface can significantly contribute to the cooling of the sharp leading edges. This project is expected to deliver new experimental data on novel surface materials exposed to a hypersonic flow environment and computer models that can simulate their cooling effect. This investigation will contribute towards enabling technologies for sustained hypersonic flight by overcoming critical head load limitations.
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    Funded Activity

    Linkage Projects - Grant ID: LP0883540

    Funder
    Australian Research Council
    Funding Amount
    $290,000.00
    Summary
    Wave slam on high speed wave piercing catamaran ferries in large seas. Australia has taken a pioneering lead in the design of high speed multi-hull ferries and continues to extend their speed, range and payload performance. Design leadership and the technology which supports it are crucial to maintaining the existing large share of the international market for such vessels. Recently freight and military transport vessels have been exposed to much more severe wave conditions than passenger vessel .... Wave slam on high speed wave piercing catamaran ferries in large seas. Australia has taken a pioneering lead in the design of high speed multi-hull ferries and continues to extend their speed, range and payload performance. Design leadership and the technology which supports it are crucial to maintaining the existing large share of the international market for such vessels. Recently freight and military transport vessels have been exposed to much more severe wave conditions than passenger vessels and this has increased the need for improved prediction of structural loads due to waves. This project directly addresses that need by computation and model testing validation. The industry is a significant export earner and employer within Australia and so the project directly underpins those national benefits.
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    Funded Activity

    Linkage Projects - Grant ID: LP0560287

    Funder
    Australian Research Council
    Funding Amount
    $356,528.00
    Summary
    Asymmetric and nonlinear unsteady loads on high speed ferries. Large high speed catamarans are expanding their domain of application from coastal passenger routes to ocean freight and military service. This is shifting operability criteria from motions and passenger discomfort to structural load limitations in severe wave environments. This project investigates large wave structural load prediction. Large waves lead to strongly non-linear responses, invalidating many methods of analysis. Predict .... Asymmetric and nonlinear unsteady loads on high speed ferries. Large high speed catamarans are expanding their domain of application from coastal passenger routes to ocean freight and military service. This is shifting operability criteria from motions and passenger discomfort to structural load limitations in severe wave environments. This project investigates large wave structural load prediction. Large waves lead to strongly non-linear responses, invalidating many methods of analysis. Prediction of loads on the transverse structure is also not possible with many prediction methods. This project will develop and validate by experiment fully time domain computational methods for the prediction of asymmetric structural loads due to large waves
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    Active Funded Activity

    Linkage Projects - Grant ID: LP200200903

    Funder
    Australian Research Council
    Funding Amount
    $933,755.00
    Summary
    Wind Tunnel Testing of a Hypersonic Plasma Engine. This project intends to evaluate an electric engine that is capable of speeds in excess of 10000 km/hr, for access to space and responsive surveillance in our region. The expertise of Lockheed Martin, Lockheed Martin Australia, the University of Qld and DST Group are to be combined to complete experimental and theoretical evaluations of an air-breathing plasma engine that is capable of out-performing rockets and scramjets. US Air Force Research .... Wind Tunnel Testing of a Hypersonic Plasma Engine. This project intends to evaluate an electric engine that is capable of speeds in excess of 10000 km/hr, for access to space and responsive surveillance in our region. The expertise of Lockheed Martin, Lockheed Martin Australia, the University of Qld and DST Group are to be combined to complete experimental and theoretical evaluations of an air-breathing plasma engine that is capable of out-performing rockets and scramjets. US Air Force Research Laboratory results will also be compared and shared. This project provides opportunities for young Australian researchers to be participate and lead an exciting new field of propulsion. It is anticipated that the program will be the foundations to future flight demonstrations from Woomera, Australia.
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