The University of Queensland

Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor

Mecklem, Sarah A., Landsberg, Will O., Curran, Damian and Veeraragavan, Ananthanarayanan (2022). Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor. Aerospace Science and Technology, 124 107551, 107551. doi: 10.1016/j.ast.2022.107551

Influence of cavity depth on ignition and flameholding modes within a scramjet combustor

Landsberg, Will O., Curran, Damian and Veeraragavan, Anand (2021). Influence of cavity depth on ignition and flameholding modes within a scramjet combustor. ASCEND 2021, Las Vegas, NV United States, 15-17 November 2021. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-4163

The Effect of Wall and Fuel Temperature in a Mach 6 Scramjet Engine

Curran, Damian, Wheatley, Vincent and Smart, Michael (2020). The Effect of Wall and Fuel Temperature in a Mach 6 Scramjet Engine. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, Australia, 7-10 December 2020. Brisbane, Australia: The University of Queensland. doi: 10.14264/7760714

Investigation of combustion mode control in a Mach 8 shape-transitioning scramjet

Curran, Damian, Wheatley, Vincent and Smart, Michael (2019). Investigation of combustion mode control in a Mach 8 shape-transitioning scramjet. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Orlando Fl, Sep 17-19, 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.j057999

Simulation of forced ignition in a Mach 6 scramjet combustor

Curran, D. R., Wheatley, V. and Smart, M. K. (2018). Simulation of forced ignition in a Mach 6 scramjet combustor. Australasian Fluid Mechanics Conference, Adelaide, Australia, 10-13 December 2018. Perth, WA, United States: Australasian Fluid Mechanics Society.

Fluid dynamic solutions to enable scramjet accelerator thrust generation from Mach 5 to 10

Curran, Damian (2021). Fluid dynamic solutions to enable scramjet accelerator thrust generation from Mach 5 to 10. PhD Thesis, School of Mechanical and Mining Engineering, Centre for Hypersonics, The University of Queensland. doi: 10.14264/91e395c

Investigation of Flow Field Manipulation, Thermal Compression and Mode Transition in a Mach 5-10 Scramjet Accelerator

Curran, Damian (2021). Investigation of Flow Field Manipulation, Thermal Compression and Mode Transition in a Mach 5-10 Scramjet Accelerator. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.

Investigation of flow field manipulation, thermal compression and mode transition in a Mach 5-10 scramjet accelerator

Curran, Damian (2021). Investigation of flow field manipulation, thermal compression and mode transition in a Mach 5-10 scramjet accelerator. PhD Thesis, School of Mechanical & Mining Engineering, The University of Queensland.

Investigation of the performance of an accelerator scramjet with CREST inlet and expansion ramp combustor

Curran, Damian (2016). Investigation of the performance of an accelerator scramjet with CREST inlet and expansion ramp combustor. Honours Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi: 10.14264/uql.2017.184