Matthew L. Fotia, Ph.D.
Affiliations: | 2012 | University of Michigan, Ann Arbor, Ann Arbor, MI |
Area:
Aerospace EngineeringGoogle:
"Matthew Fotia"Parents
Sign in to add mentor| James F. Driscoll | grad student | 2012 | University of Michigan | |
| (Experimental Study of Shock-train/Combustion Coupling and Flame Dynamics in a Heated Supersonic Flow.) | ||||
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Publications
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| Huff R, Polanka MD, McClearn MJ, et al. (2019) Design and Operation of a Radial Rotating Detonation Engine Journal of Propulsion and Power. 35: 1143-1150 |
| Rankin BA, Fotia ML, Naples AG, et al. (2017) Overview of Performance, Application, and Analysis of Rotating Detonation Engine Technologies Journal of Propulsion and Power. 33: 131-143 |
| Kaemming TA, Fotia M, Hoke J, et al. (2017) Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced-Order Approach Journal of Propulsion and Power. 33: 1170-1178 |
| Fotia ML, Hoke J, Schauer F. (2017) Experimental Performance Scaling of Rotating Detonation Engines Operated on Gaseous Fuels Journal of Propulsion and Power. 33: 1187-1196 |
| Fotia ML, Schauer F, Kaemming T, et al. (2016) Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle Journal of Propulsion and Power. 32: 674-681 |
| Fotia ML. (2015) Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet–Scramjet Experiment Journal of Propulsion and Power. 31: 69-78 |
| Fotia ML, Driscoll JF. (2013) Ram-Scram Transition and Flame/Shock-Train Interactions in a Model Scramjet Experiment Journal of Propulsion and Power. 29: 261-273 |
| Fotia ML, Driscoll JF. (2012) Isolator-Combustor Interactions in a Direct-Connect Ramjet-Scramjet Experiment Journal of Propulsion and Power. 28: 83-95 |
| Torrez SM, Driscoll JF, Ihme M, et al. (2011) Reduced-order modeling of turbulent reacting flows with application to ramjets and scramjets Journal of Propulsion and Power. 27: 371-382 |
| Dalle DJ, Fotia ML, Driscoll JF. (2010) Reduced-Order Modeling of Two-Dimensional Supersonic Flows with Applications to Scramjet Inlets Journal of Propulsion and Power. 26: 545-555 |