Onset Theory: Pushing the design envelope for textile composite structures. This study aims to exploit an innovative physics-based approach to predict the strength of textile composites. This is particularly important in areas such as aircraft design, where drastic weight savings are needed to allow designers to remain competitive in a low-carbon future. Improved theory and design tools will remove conservatism and account for a large part of these weight savings. The new approach is the first t ....Onset Theory: Pushing the design envelope for textile composite structures. This study aims to exploit an innovative physics-based approach to predict the strength of textile composites. This is particularly important in areas such as aircraft design, where drastic weight savings are needed to allow designers to remain competitive in a low-carbon future. Improved theory and design tools will remove conservatism and account for a large part of these weight savings. The new approach is the first to be consistent at all length scales — from atoms to aeroplanes — ensuring relevance for new and evolving composite material systems. A novel understanding of crack initiation in textile laminates is intended to reduce design and certification effort for new aircraft and help to design more efficient airframes at a lower cost.Read moreRead less
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.Read moreRead less
AM of MAX Phase parts for applications in extreme environments. This project aims to develop techniques to synthesize MAX Phase compound materials in-situ using laser additive manufacturing. The project expects to increase jet engine fuel efficiency and thrust, and to fabricate longer-lasting parts for supersonic speed applications. The expected outcomes include well-developed additive manufacturing processes to make high performance engineering components with shape complexity for extreme envir ....AM of MAX Phase parts for applications in extreme environments. This project aims to develop techniques to synthesize MAX Phase compound materials in-situ using laser additive manufacturing. The project expects to increase jet engine fuel efficiency and thrust, and to fabricate longer-lasting parts for supersonic speed applications. The expected outcomes include well-developed additive manufacturing processes to make high performance engineering components with shape complexity for extreme environment applications, and new methods to increase the 3D printability of brittle materials. This should provide significant benefits to aerospace and defense industries through solving their long standing bottleneck material and processing problems. The outcomes also enhance Australia’s manufacturing capacity.Read moreRead less
Discovery Early Career Researcher Award - Grant ID: DE120102277
Funder
Australian Research Council
Funding Amount
$375,000.00
Summary
Design optimisation and physical behaviour of fuel injection and mixing for innovative scramjet concepts. Scramjets are a potential game changer for satellite launch and high speed flight. The phenomena that will make or break them are complex, and achieving optimal designs is hugely challenging. This project combines advanced optimisation techniques and flow simulations to find, and understand, optimal fuel injection for innovative scramjet designs.
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE120100139
Funder
Australian Research Council
Funding Amount
$350,000.00
Summary
A Hot Isostatic Press (HIP) for aerospace and biomedical component processing. This facility will provide a hot isostatic press of sufficiently large capacity to maximise production efficiencies in aerospace and biomedical applications through net shape manufacturing. The facility will be able to process small components or prototypes which will behave in a manner similar to larger scale components.
Are some languages better than others? It is important for the Australian community - speaking several hundred different indigenous and immigrant languages across the nation - to realise that each language has approximately (but not precisely) the same overall complexity as every other. One may have intricate word structure, while another has short words but elaborate rules for putting words together to make sentences. And, striding above 'political correctness', many people in Australia will be ....Are some languages better than others? It is important for the Australian community - speaking several hundred different indigenous and immigrant languages across the nation - to realise that each language has approximately (but not precisely) the same overall complexity as every other. One may have intricate word structure, while another has short words but elaborate rules for putting words together to make sentences. And, striding above 'political correctness', many people in Australia will be interested to know whether a certain language is a little more efficient than certain other languages for a particular purpose (for example, commercial business). Read moreRead less
Theoretical model that predicts the grain size of alloys inoculated with micro- and nano- particle master alloys and cast under an external field. The aim of this project is to develop a theoretical model that predicts grain size when components are cast under the influence of external fields (electromagnetic, ultrasonic, pulsed electric current and melt shearing treatments) and with the addition of nano-particle master alloys. Refining microstructures by available master alloys is reaching a li ....Theoretical model that predicts the grain size of alloys inoculated with micro- and nano- particle master alloys and cast under an external field. The aim of this project is to develop a theoretical model that predicts grain size when components are cast under the influence of external fields (electromagnetic, ultrasonic, pulsed electric current and melt shearing treatments) and with the addition of nano-particle master alloys. Refining microstructures by available master alloys is reaching a limit and this limits further improvement in mechanical properties to meet the challenge of new applications requiring, for example, high temperature properties or light weighting (for example, use of less material). The outcomes will be a new theoretical model, validated numerical models, new casting technologies and highly refined alloys with greater than 25 per cent improvement in mechanical properties. Read moreRead less
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.Read moreRead less
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE110100059
Funder
Australian Research Council
Funding Amount
$500,000.00
Summary
Vacuum induction furnace for casting titanium alloys. This titanium melting facility will provide a level of investment and national strategic focus necessary to sustain Australian competitive advantage in both titanium research and the global titanium market. The facility will support cutting-edge research and support the development of new titanium products.