Dr Jens Kunze
Postdoctoral Research Fellow
School of Mechanical and Mining Engineering
Journal Articles
Kunze, Jens and Paull, Allan (2023). Preliminary analysis of the performance of an electric supersonic propeller. Aerospace, 10 (9) 803, 803. doi: 10.3390/aerospace10090803
Kunze, Jens, Smart, Michael K. and Gollan, Rowan (2022). A design method for three-dimensional scramjet nozzles with shape transition. Journal of Propulsion and Power, 38 (1), 3-17. doi: 10.2514/1.b38293
Conference Papers
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
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
Kunze, Jens, Smart, Michael K. and Gollan, Rowan (2018). A design method for elliptical to rectangular shape transition nozzles. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, September 17, 2018-September 19, 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-5318
Data Collection
Kunze, Jens and Paull, Allan (2023). Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller. The University of Queensland. (Dataset) doi: 10.48610/9292b60
Theses
Kunze, Jens (2020). Design of a 3D shape transitioning nozzle and experimental thrust measurements of an airframe integrated scramjet. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi: 10.14264/uql.2020.182
Kunze, Jens (2014). Entwicklung von dreidimensionalen Düsen mit sich von elliptisch auf rechteckig änderndem Querschnitt. Master's Thesis, Institute for Flight Propulsion, TU Munich, Technical University of Munich.