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2024

Conference Publication

STAJe<sup>-</sup>: A Supersonic Flight Program STAJe-1 Payload Design and System Study

Kunze, Jens, Shelar, Sampada Vijay and Paull, Allan (2024). STAJe-: A Supersonic Flight Program STAJe-1 Payload Design and System Study. AIAA Aviation Forum and Exposition (AIAA Aviation Forum), Chicago, IL United States, 27 June - 1 July 2022. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.A35544

STAJe<sup>-</sup>: A Supersonic Flight Program STAJe-1 Payload Design and System Study

2023

Conference Publication

System Overview of the STAJe<sup>-</sup> 1 Payload

Kunze, Jens and Paull, Allan (2023). System Overview of the STAJe- 1 Payload. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Karnataka, India, 28 May - 1 June 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-3004

System Overview of the STAJe<sup>-</sup> 1 Payload

2015

Conference Publication

A concept for the HiFIRE 8 flight test

Alesi, Hans, Paull, Allan, Smart, Michael and Bowcutt, Kevin G. (2015). A concept for the HiFIRE 8 flight test. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, Tromso, Norway, 7-12 June 2015. Noordwijk, The Netherlands: ESA Communications.

A concept for the HiFIRE 8 flight test

2013

Conference Publication

Ethylene augmentation of JP-8+100 in a supersonic combustor

Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, 14-17 July, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3700

Ethylene augmentation of JP-8+100 in a supersonic combustor

2012

Conference Publication

HIFiRE: an international collaboration to advance the science and technology of hypersonic flight

Bowcutt, Kevin, Paull, Alan, Dolvin, Douglas and Smart, Michael (2012). HIFiRE: an international collaboration to advance the science and technology of hypersonic flight. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, QLD, Australia, 23-28 September 2012. Bonn, Germany: International Council of the Aeronautical Sciences (ICAS).

HIFiRE: an international collaboration to advance the science and technology of hypersonic flight

2009

Conference Publication

Aerodynamic design of hypersonic re-entry flight HIFiRE 7

Eggers, Thino, Silvester, Todd B., Paull, Allan and Smart, Michael K. (2009). Aerodynamic design of hypersonic re-entry flight HIFiRE 7. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19 - 22 October 2009. Reston, VA United States: AIAA. doi: 10.2514/6.2009-7256

Aerodynamic design of hypersonic re-entry flight HIFiRE 7

2009

Conference Publication

Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming

Hunt, D. C., Paull, A., Boyce, R. R. and Hagenmaier, M. (2009). Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming. 19th International Symposium on Airbreathing Engines (ISABE2009), Montreal, Canada, 7-11 September, 2009. Montreal, Canada: ISABE.

Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming

2007

Conference Publication

Hypersonics Research in Australia

Morgan, Richard, Paull, Allan, Smart, Michael and Stalker, Ray (2007). Hypersonics Research in Australia. AVT-150 RTO AVT/VKI Lecture Series: Advances on Propulsion Technology for High-Speed Aircraft, Von Karmen Institute for Fluid Mechanics, Rhode St. Genese, Belgium, 12-15 March 2007. Neuilly-sur-Seine, France: NATO Research and Technology Organisation.

Hypersonics Research in Australia

2007

Conference Publication

Radical farming in scramjets

Odaml J. and Paull A. (2007). Radical farming in scramjets. doi: 10.1007/978-3-540-74460-3_34

Radical farming in scramjets

2006

Conference Publication

Experiments on external combustion with leading edge fuel-injection in hypersonic flow

Coras, Samantha and Paull, Allan (2006). Experiments on external combustion with leading edge fuel-injection in hypersonic flow.

Experiments on external combustion with leading edge fuel-injection in hypersonic flow

2006

Conference Publication

Development of the HyShot stability demonstrator

Neuenhahn, Thomas, Olivier, Herbert and Paull, Allan (2006). Development of the HyShot stability demonstrator.

Development of the HyShot stability demonstrator

2006

Conference Publication

Development of the Hyshot Stability Demonstrator

Neuenhahn, T, Olivier, H and Paull, A (2006). Development of the Hyshot Stability Demonstrator. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, California, USA, 5-8 June 2006. USA: American Institute of Aeronautics and Astronautics.

Development of the Hyshot Stability Demonstrator

2006

Conference Publication

Imaging of hydrogen fuel injection on the intake of a heated wall scramjet

Kovachevich, Anne L., Hajek, Kim M., McIntyre, Timothy J., Paull, Allan and Abdel-Jawad, Madhat (2006). Imaging of hydrogen fuel injection on the intake of a heated wall scramjet. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Sacramento, California, 9 - 12 July 2006. AIAA.

Imaging of hydrogen fuel injection on the intake of a heated wall scramjet

2006

Conference Publication

Experiments on external combusion with leading edge fuel-injection in hypersonic flow

Coras, S. J. and Paull, A (2006). Experiments on external combusion with leading edge fuel-injection in hypersonic flow. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics.

Experiments on external combusion with leading edge fuel-injection in hypersonic flow

2005

Conference Publication

Flight data analysis of HyShot 2

Mass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight data analysis of HyShot 2.

Flight data analysis of HyShot 2

2005

Conference Publication

Performance of a scramjet combustor with combined normal and tangential fuel injection

Rowan, Scott A. and Paull, Allan (2005). Performance of a scramjet combustor with combined normal and tangential fuel injection. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2005-615

Performance of a scramjet combustor with combined normal and tangential fuel injection

2005

Conference Publication

A 256 channel high speed modular flight computer for hypersonic launch vehicles

Finlayson, Simon and Paull, Allan (2005). A 256 channel high speed modular flight computer for hypersonic launch vehicles.

A 256 channel high speed modular flight computer for hypersonic launch vehicles

2005

Conference Publication

Flight Data Analysis of HyShot 2

Hass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight Data Analysis of HyShot 2. 13th AIAA/CIRA International Space Planes and Hypersonic Systems Technologies Conference, Capua, Italy, 16-20 May 2005. Hampton, Virginia, U.S.A.: NASA Langley Research Center.

Flight Data Analysis of HyShot 2

2005

Conference Publication

Operating conditions in UQ's impulse facilities for scramjet testing

McGilvray, M., Morgan, R. G., Paull, A., Abdel-Jawad, M. M., Jacobs, P. A., McIntyre, T. J. and Scott, M. A. (2005). Operating conditions in UQ's impulse facilities for scramjet testing. 25th International Symposium on Shock Waves, Bangalore, India, 17-22 July 2005.

Operating conditions in UQ's impulse facilities for scramjet testing

2004

Conference Publication

Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data

Gardner, A. D., Hannemann, K., Steelant, J. and Paull, A. (2004). Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2004-3345

Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data