Experimental Comparison of Temperature Distribution and Heat Recirculation Values for Propane and Methane Premixed Flames in a Simulated Microcombustor Using Non-Intrusive FTIR Diagnostics
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American Institute of Aeronautics and Astronautics
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1. A six-wafer combustion system for a silicon micro gas turbine engine
2. Analysis of non-adiabatic heat-recirculating combustors
3. Influence of conductive heat-losses on the propagation of premixed flames in channels
4. The role of structural heat exchange and heat loss in the design of efficient silicon micro-combustors
5. Theoretical and experimental studies on mesoscale flame propagation and extinction
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