Understanding flapping aerodynamics in non-optimal environments. This project aims to produce a deeper understanding of factors affecting the aerodynamic forces and detailed flow dynamics of a flapping insect-like wing over a multi-dimensional parameter space with an initial focus on micro-air vehicles. The project will determine the effects of oncoming flow uniformities and environmental factors on flight performance, and how to correct for these factors to stabilise flight using feedback contr ....Understanding flapping aerodynamics in non-optimal environments. This project aims to produce a deeper understanding of factors affecting the aerodynamic forces and detailed flow dynamics of a flapping insect-like wing over a multi-dimensional parameter space with an initial focus on micro-air vehicles. The project will determine the effects of oncoming flow uniformities and environmental factors on flight performance, and how to correct for these factors to stabilise flight using feedback control. The project will use advanced computational and experimental modelling and analysis to provide specific design guidance and strategies for very-small and highly functional micro air vehicles for wide ranging applications in areas including transport, marine engineering and sport.Read moreRead less
Discovery Early Career Researcher Award - Grant ID: DE140101546
Funder
Australian Research Council
Funding Amount
$288,900.00
Summary
Development of computer-based optimisation to improve hypersonic aerodynamic design. Next-generation launch vehicles using high-speed jet engines will make it cheaper and more reliable for humankind to engage in activities in space. This project will contribute to the technology of high-speed jet engines by developing optimised air intake systems. The research aims to advance the use of computational engineering and apply this to improve the design of air intake systems. The outcomes of this pro ....Development of computer-based optimisation to improve hypersonic aerodynamic design. Next-generation launch vehicles using high-speed jet engines will make it cheaper and more reliable for humankind to engage in activities in space. This project will contribute to the technology of high-speed jet engines by developing optimised air intake systems. The research aims to advance the use of computational engineering and apply this to improve the design of air intake systems. The outcomes of this project will advance the technology of high-speed jet engines with the goal of replacing existing rocket systems.Read moreRead less
Magnetohydrodynamic Aerobraking for Spacecraft Entry to Earth's Atmosphere. A spaceship returning from Mars will undergo unprecedented aerodynamic heating as it enters Earth's atmosphere. Magnetohydroynamic aerobraking involves applying a strong magnetic field to the plasma which forms around the spacecraft at these speeds, theoretically protecting it by reducing structural heat loads and enabling less severe flight trajectories. This project aims to experimentally study this technology for Eart ....Magnetohydrodynamic Aerobraking for Spacecraft Entry to Earth's Atmosphere. A spaceship returning from Mars will undergo unprecedented aerodynamic heating as it enters Earth's atmosphere. Magnetohydroynamic aerobraking involves applying a strong magnetic field to the plasma which forms around the spacecraft at these speeds, theoretically protecting it by reducing structural heat loads and enabling less severe flight trajectories. This project aims to experimentally study this technology for Earth return from deep space. It is significant because it will evaluate a new mechanism for managing the tremendous heat loads of planetary entry. The expected outcome and benefit will be development of a new technology to reduce spacecraft heating, leading to safer, more efficient, and potentially reusable spacecraft.Read moreRead less