The mechanics of quiet airfoils. Airfoil trailing edge noise affects many technologies, from wind turbines to computer cooling fans and must be reduced to improve productivity, public health and the environment. This project aims to develop a new class of quiet airfoil design and an active trailing edge noise control system to help solve this important problem. This research will provide multiple, long terms benefits to Australia that include reduced greenhouse gas emissions, reduced airport no ....The mechanics of quiet airfoils. Airfoil trailing edge noise affects many technologies, from wind turbines to computer cooling fans and must be reduced to improve productivity, public health and the environment. This project aims to develop a new class of quiet airfoil design and an active trailing edge noise control system to help solve this important problem. This research will provide multiple, long terms benefits to Australia that include reduced greenhouse gas emissions, reduced airport noise, new high technology products for export, and improved public health.Read moreRead less
Development of an active noise control system for sleeper seats on large commercial aircraft. Possible avenues will be investigated to actively reduce aircraft cabin noise experienced by passengers in sleeper seats, using localised active noise control (ANC). Previous work has focused on headsets and upright seat headrests which represent a different problem to the partially enclosed sleeper seats considered here. Efficiency and robustness problems that affect existing ANC systems will be addres ....Development of an active noise control system for sleeper seats on large commercial aircraft. Possible avenues will be investigated to actively reduce aircraft cabin noise experienced by passengers in sleeper seats, using localised active noise control (ANC). Previous work has focused on headsets and upright seat headrests which represent a different problem to the partially enclosed sleeper seats considered here. Efficiency and robustness problems that affect existing ANC systems will be addressed. A prototype system will be produced for a business class sleeper seat in a wide body aircraft. A second outcome is the establishment of a robust integrated system design procedure that can be used to quickly develop ANC systems for future designs.Read moreRead less
Linkage Infrastructure, Equipment And Facilities - Grant ID: LE0560673
Funder
Australian Research Council
Funding Amount
$377,178.00
Summary
Scanning 3D laser vibrometer for non-contact in-plane and out-of-plane vibration measurement. The requested 3D scanning laser vibrometer is intended for the characterisation of 3D vibration of small and large, simple and complex structures, for the purpose of understanding the vibratory behaviour as a precursor to optimising noise and vibration control strategies. It has application to small items for which the use of contact sensors is impossible or impractical, as well as large structures for ....Scanning 3D laser vibrometer for non-contact in-plane and out-of-plane vibration measurement. The requested 3D scanning laser vibrometer is intended for the characterisation of 3D vibration of small and large, simple and complex structures, for the purpose of understanding the vibratory behaviour as a precursor to optimising noise and vibration control strategies. It has application to small items for which the use of contact sensors is impossible or impractical, as well as large structures for which the vibration fields can be complex and a 3D scanning capability is essential. Examples include micro-positioning actuators, piezo-electric motors, live cell response, disk brakes, aircraft and vehicles. Outcomes include the enhancement of existing research projects, allowing a greater understanding of the noise and vibration phenomena.Read moreRead less
A theoretical investigation into the effect of nonlinear wave interactions in promoting transition-to-turbulence. The problem of transition-to-turbulence remains one of the fundamental unanswered questions in fluid dynamics. An understanding of the processes leading to transition is necessary if the active control of turbulence is to be achieved. This project will focus attention on a new class of waves, which have only recently been described the CI, in order to determine how they are triggered ....A theoretical investigation into the effect of nonlinear wave interactions in promoting transition-to-turbulence. The problem of transition-to-turbulence remains one of the fundamental unanswered questions in fluid dynamics. An understanding of the processes leading to transition is necessary if the active control of turbulence is to be achieved. This project will focus attention on a new class of waves, which have only recently been described the CI, in order to determine how they are triggered and how they may serve to actively promote the early development of turbulence in a broad class of fluid flows.Read moreRead less
Optimal nose shaping for delayed boundary-layer separation and transition in axisymmetric flow. The aim of this project is to design a smooth nose for a body of revolution placed in axisymmetric flow of a viscous fluid at high Reynolds number, such that the boundary layer on the body remains unseparated. This can always be done with a sufficiently long nose, but our objective here is to minimise the necessary nose length. Outer potential flows will be provided via ring sources. The potential flo ....Optimal nose shaping for delayed boundary-layer separation and transition in axisymmetric flow. The aim of this project is to design a smooth nose for a body of revolution placed in axisymmetric flow of a viscous fluid at high Reynolds number, such that the boundary layer on the body remains unseparated. This can always be done with a sufficiently long nose, but our objective here is to minimise the necessary nose length. Outer potential flows will be provided via ring sources. The potential flows will be used to determine inner boundary layer solutions. Transition-to-turbulence will be considered by undertaking 2D and 3D stability computations.Read moreRead less
Evaluation of a Fatigue Risk Management System in the Australian aviation industry. The proposed project will develop and validate tools and guidance materials for design and implementation fatigue risk management systems [FRMSs]. Upon completion of the project, these tools will be made freely available to CASA and the Australian aviation industry. This will assist CASA in providing an efficient FRMS implementation strategy that has been scientifically validated. Furthermore, it will improve ....Evaluation of a Fatigue Risk Management System in the Australian aviation industry. The proposed project will develop and validate tools and guidance materials for design and implementation fatigue risk management systems [FRMSs]. Upon completion of the project, these tools will be made freely available to CASA and the Australian aviation industry. This will assist CASA in providing an efficient FRMS implementation strategy that has been scientifically validated. Furthermore, it will improve safety and minimise the cost of FRMS design and implementation to the aviation industry, which has recently undergone significant financial burden. Ultimately, this will improve safety for the flying public. Read moreRead less
How tired is too tired? Determining the effects of fatigue on pilots' performance in a simulated flight environment. Increasingly, pilots are required to work more flexible flight schedules that expose them to greater levels of work-related fatigue. Consequently, a recent federal parliamentary inquiry recommended that a fatigue risk management approach be applied to the regulation of pilots? flight and duty times. A key aspect of such an approach, and the aim of the proposed project, is to det ....How tired is too tired? Determining the effects of fatigue on pilots' performance in a simulated flight environment. Increasingly, pilots are required to work more flexible flight schedules that expose them to greater levels of work-related fatigue. Consequently, a recent federal parliamentary inquiry recommended that a fatigue risk management approach be applied to the regulation of pilots? flight and duty times. A key aspect of such an approach, and the aim of the proposed project, is to determine the level of fatigue at which pilots? ability to operate an aircraft reaches a safety-critical level. This research will provide a scientifically validated benchmark for regulating pilots? flight and duty times. Ultimately, this will improve safety for the flying public.Read moreRead less