Research Output per year
Research Output per year
Personal profile
Biography
Daniel Edgington-Mitchell received his undergraduate degrees in Mechanical and Aerospace Engineering from Monash University in 2005. During his PhD, he undertook graduate research in the High Temperature Gas Dynamics Laboratory at Stanford University under the auspices of a Fulbright Fellowship between 2008-2009. He was awarded his PhD from Monash University in 2013. He now works as a lecturer in the Department of Mechanical and Aerospace Engineering at Monash University, and as a researcher in the Laboratory for Turbulence Research in Aerospace and Combustion.
You can visit his website at daniel.edgington-mitchell.com
Research area keywords
- Aeroacoustics
- Fluid Mechanics
- High speed propulsion
- Jet noise
Network
Recent external collaboration on country level. Dive into details by clicking on the dots.
Research Output
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Azimuthal decomposition of the radiated noise from supersonic shock-containing jets
Wong, M. H., Kirby, R., Jordan, P. & Edgington-Mitchell, D., 1 Oct 2020, In : Journal of the Acoustical Society of America. 148, 4, p. 2015-2027 13 p.Research output: Contribution to journal › Article › Research › peer-review
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Characteristics of acoustic and hydrodynamic waves in under-expanded supersonic impinging jets
Karami, S., Edgington-Mitchell, D., Theofilis, V. & Soria, J., 25 Dec 2020, In : Journal of Fluid Mechanics. 905, 33 p., A34.Research output: Contribution to journal › Article › Research › peer-review
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Dynamic evolution of a transient supersonic trailing jet induced by a strong incident shock wave
Rezay Haghdoost, M., Edgington-Mitchell, D., Nadolski, M., Klein, R. & Oberleithner, K., Jul 2020, In : Physical Review Fluids. 5, 7, 23 p., 073401.Research output: Contribution to journal › Article › Research › peer-review
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Evaluation of shock dividers using numerical and experimental methods
Haghdoost, M. R., Thethy, B. S., Nadolski, M., Klein, R., Honnery, D., Edgington-Mitchell, D., Seo, B., Paschereit, C. O. & Oberleithner, K., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 19 p. (AIAA Scitech 2020 Forum; vol. 1 PartF).Research output: Chapter in Book/Report/Conference proceeding › Conference Paper › Other
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High-speed schlieren and particle image velocimetry of the exhaust flow of a pulse detonation combustor
Haghdoost, M. R., Edgington-Mitchell, D., Paschereit, C. O. & Oberleithner, K., Aug 2020, In : AIAA Journal. 58, 8, p. 3527-3543 17 p.Research output: Contribution to journal › Article › Research › peer-review
1 Citation (Scopus)