Measurement of Aerothermal Heating on HIFiRE-0
Paper
Neely, Andrew J., Choudhury, Rishabh, Paukner, Daniel and Odam, Judy. 2011. "Measurement of Aerothermal Heating on HIFiRE-0." 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (2011). United States 11 - 14 Apr 2011 United States. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2356
| Paper/Presentation Title | Measurement of Aerothermal Heating on HIFiRE-0 |
|---|---|
| Presentation Type | Paper |
| Authors | Neely, Andrew J., Choudhury, Rishabh, Paukner, Daniel and Odam, Judy |
| Journal or Proceedings Title | Proceedings of the 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (2011) |
| Article Number | 2011-2356 |
| Year | 2011 |
| Publisher | American Institute of Aeronautics and Astronautics |
| Place of Publication | United States |
| ISBN | 9781600869426 |
| Digital Object Identifier (DOI) | https://doi.org/10.2514/6.2011-2356 |
| Web Address (URL) of Paper | https://arc.aiaa.org/doi/abs/10.2514/6.2011-2356 |
| Conference/Event | 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (2011) |
| Event Details | 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (2011) Parent AIAA International Space Planes and Hypersonic Systems and Technologies Conference Delivery Online Event Date 11 to end of 14 Apr 2011 Event Location United States |
| Abstract | Patches of permanent-change thermal paint were flown on DSTO's HIFiRE-0 hypersonic test vehicle. HIFiRE-0 was used as an engineering development and risk reduction flight for the fundamental science payload, HIFiRE 1 and subsequent flights in the HIFiRE series. Permanent-change thermal paint was applied to sections of the stainless steel nose cone, both externally and internally and to the aluminium instrumentation can. These paints were applied as an initial test of their suitability to measure the distribution of heating for a highly transient flight profile. After post-flight recovery of the payload, regions of the applied thermal paint were still clearly visible and had undergone a noticeable colour change due to inflight heating. Transient CFD simulations of the ascent and descent of the vehicle through the atmosphere, which incorporated conjugate heat transfer provided reasonable predicts of the observed paint colour change in the region investigated. © 2011 by Andrew J. Neely. |
| Keywords | Aerothermal heating; CFD simulations; Colour change; Conjugate heat transfer; Engineering development; Flight profiles; Risk reductions; Thermal paints |
| Public Notes | There are no files associated with this item. |
| Funder | U.S. Air Force |
| Byline Affiliations | University of New South Wales |
| Technical University of Munich, Germany | |
| Department of Defence, Australia | |
| Library Services |
Permalink -
https://research.usq.edu.au/item/wqvz1/measurement-of-aerothermal-heating-on-hifire-0
44
total views0
total downloads3
views this month0
downloads this month
Export as
Related outputs
Hypersonic Pitching Control Model Development
Stern, Nathan, Buttsworth, David, Choudhury, Rishabh and Birch, Byrenn. 2018. "Hypersonic Pitching Control Model Development." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 Reston, United States. https://doi.org/10.2514/6.2018-5267Pressure Fluctuations in a Hypersonic Ludwieg Tube with Free Piston Compression Heating
Birch, Byrenn J. C., Choudhury, Rishabh, Stern, Nathan and Buttsworth, David R.. 2018. "Pressure Fluctuations in a Hypersonic Ludwieg Tube with Free Piston Compression Heating." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 Reston, United States. https://doi.org/10.2514/6.2018-5266Analysis of Reentry and Break-Up Forces from Impulse Facility Experiments and Numerical Rebuilding
Leiser, David, Loehle, Stefan, Zander, Fabian, Buttsworth, David R., Choudhury, Rishabh and Fasoulas, Stefanos. 2022. "Analysis of Reentry and Break-Up Forces from Impulse Facility Experiments and Numerical Rebuilding." Journal of Spacecraft and Rockets. 59 (4), pp. 1276-1288. https://doi.org/10.2514/1.A35204Hypersonic oscillating shock-wave/boundary-layer interaction on a flat plate
Currao, Gaetano M. D., McQuellin, Liam P., Neely, Andrew J., Gai, Sudhir L., O'Byrne, Sean, Zander, Fabian, Buttsworth, David R., McNamara, Jack J. and Jahn, Ingo. 2021. "Hypersonic oscillating shock-wave/boundary-layer interaction on a flat plate." AIAA Journal: devoted to aerospace research and development. 59 (3), pp. 940-959. https://doi.org/10.2514/1.J059590An Experimental and Numerical Investigation into the Aerodynamics of the ISS Re-entry
Zander, F., Leiser, D., Choudhury, R., Loehle, S. and Buttsworth, D.R.. 2018. "An Experimental and Numerical Investigation into the Aerodynamics of the ISS Re-entry." Lau, T.C.W. and Kelso, R.M. (ed.) 21st Australasian Fluid Mechanics Conference (AFMC 2018). Adelaide, Australia 10 - 13 Dec 2018 Australia. Australasian Fluid Mechanics Society.Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Supersonic combustion of hydrogen in Mach 2 flows over an axisymmetric model." 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference (AIAA 2018). Orlando, United States 17 - 19 Sep 2018 United States. https://doi.org/10.2514/6.2018-5252Aerodynamic database of the HEXAFLY‑INT hypersonic glider
Schettino, Antonio, Pezzella, Giuseppe, Marini, Marco, Di Benedetto, Sara, Villace, Victor F., Steelant, Johan, Choudhury, Rishabh, Gubanov, Anatoly and Voevodenko, Nina. 2020. "Aerodynamic database of the HEXAFLY‑INT hypersonic glider." CEAS Space Journal. 12 (2), pp. 295-311. https://doi.org/10.1007/s12567-020-00299-4Measurement of water vapour in axisymmetric jet development using TDLAS
Al-Manea, A., Buttsworth, D., Leis, J., Choudhury, R. and Saleh, K.. 2018. "Measurement of water vapour in axisymmetric jet development using TDLAS." Lau, T. C. W. and Kelso, R. M. (ed.) 21st Australasian Fluid Mechanics Conference (AFMC 2018). Adelaide, Australia 10 - 13 Dec 2018 Australia. Australasian Fluid Mechanics Society.Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames
Zhao, Mengmeng, Buttsworth, David and Choudhury, Rishabh. 2018. "Experimental and numerical study of OH* chemiluminescence in hydrogen diffusion flames." Combustion and Flame. 197, pp. 369-377. https://doi.org/10.1016/j.combustflame.2018.08.019Oscillating shock impinging on a flat plate at Mach 6
Currao, Gaetano M. D., McQuellin, Liam P., Neely, Andrew J., Zander, Fabian, Buttsworth, David R., McNamara, Jack J. and Jahn, Ingo. 2019. "Oscillating shock impinging on a flat plate at Mach 6." AIAA Aviation Forum 2019. Dallas, United States 17 - 21 Jun 2019 United States. https://doi.org/10.2514/6.2019-3077Spacecraft Material Tests under Aerothermal and Mechanical Reentry Loads
Leiser, David, Lohle, Stefan, Zander, Fabian, Fasoulas, Stefanos, Buttsworth, David R. and Choudhury, Rishabh. 2019. "Spacecraft Material Tests under Aerothermal and Mechanical Reentry Loads." AIAA SciTech Forum 2019 . San Diego, United States 07 - 11 Jan 2019 United States. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-0161Study of an axisymmetric backward facing step model in a supersonic flow
Zhao, Mengmeng, Buttsworth, David R., Choudhury, Rishabh, Malpress, Ray and Xing, Fei. 2016. "Study of an axisymmetric backward facing step model in a supersonic flow." 21st AIAA International Space Planes and Hypersonics Technologies Conference (Hypersonics 2017). Xiamen, China 06 - 09 Mar 2017 United States. https://doi.org/10.2514/6.2017-2181Two way coupled hypersonic fluid structure interaction simulations with Eilmer
Jahn, I.H.J., Currao, G.M.D., Neely, A.J., Gollan, R. and Jacobs, P.. 2018. "Two way coupled hypersonic fluid structure interaction simulations with Eilmer." 21st Australasian Fluid Mechanics Conference (AFMC 2018). Adelaide, Australia 10 - 13 Dec 2018 Australia. Australasian Fluid Mechanics Society.Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model
Zhao, M. M., Choudhury, R., Malpress, R. and Buttsworth, D. R.. 2016. "Absolute concentration measurements of OH* in an axisymmetric hydrogen-air premixed flame adjacent to a hot graphite model." 20th Australasian Fluid Mechanics Conference (AFMC 2016). Perth, Australia 05 - 08 Dec 2016 Australia.Hypersonic wind-tunnel free-flying experiments with onboard instrumentation
Mudford, Neil R., O'Byrne, Sean, Neely, Andrew, Buttsworth, David and Balage, Sudantha. 2015. "Hypersonic wind-tunnel free-flying experiments with onboard instrumentation." Journal of Spacecraft and Rockets. 52 (1), pp. 231-242. https://doi.org/10.2514/1.A32887A new method for prescribing non-uniform wall temperatures on wind tunnel models
Neely, A. J., Dasgupta, A. and Choudhury, R.. 2014. "A new method for prescribing non-uniform wall temperatures on wind tunnel models." 19th Australasian Fluid Mechanics Conference (AFMC 2014). Melbourne, Australia 08 - 11 Dec 2014 Australia.Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight
Choudhury, Rishabh and Neely, Andrew J.. 2012. "Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight." 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012). Tours, France 24 - 28 Sep 2012 United States. https://doi.org/10.2514/6.2012-5899Thermal-structural modelling of TDLAS system for SCRAMSPACE hypersonic flight test
Dasgupta, Arnab, Choudhury, Rishabh, Neely, Andrew, O'Byrne, Sean and Kurtz, Joe. 2012. "Thermal-structural modelling of TDLAS system for SCRAMSPACE hypersonic flight test." 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference (AIAA 2012). Tours, France 24 - 28 Sep 2012 United States.Super-orbital re-entry in Australia: laboratory measurement, simulation and flight observation [Keynote lecture]
Buttsworth, David, Jacobs, Peter, Potter, Daniel, Mudford, Neil, D'Souza, Mary, Eichmann, Troy, Jenniskens, Peter, McIntyre, Tim, Jokic, Michael, Jacobs, Carolyn, Upcroft, Ben, Khan, Razmi, Porat, Hadas, Neely, Andrew and Lohle, Stefan. 2012. "Super-orbital re-entry in Australia: laboratory measurement, simulation and flight observation [Keynote lecture]." Kontis, Konstantinos (ed.) 28th International Symposium on Shock Waves (ISSW 28). Manchester, United Kingdom 17 - 22 Jul 2011 Heidelberg, Germany. https://doi.org/10.1007/978-3-642-25688-2_5Hypersonic Drop-Tests of a Sphere: CFD Comparison to Experimental Results
Choudhury, R., Doig, G., Neely, A. and Barber, T.. 2010. "Hypersonic Drop-Tests of a Sphere: CFD Comparison to Experimental Results." 17th Australasian Fluid Mechanics Conference (AFMC 2010). Auckland, New Zealand 05 - 09 Dec 2010 New Zealand. pp. 465-468This item comprises data from the following sources: Scopus