Chi-Ming Lee Chief of Combustion Branch NASA Glenn Research ...

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Concentration 0 Time--> C 7 C 8 Fischer-Tropsch & JP-8 Fuel Analysis C 8 C 9 C 10 C 11 C 12 C 13 C 14 C 15 C 16 C 17 5 10 15 20 25 30 Time C 18 Shell F-T JP-8 C 19 12
JP8, 50-50 Blend, and FT-2 Comparisons Video Images, with flow from left to right Comparison showing average flame length and luminous intensity for T3 = 1030°F 13
Page 1 and 2: Chi-Ming Lee Chief of Combustion Br
Page 3 and 4: NOx emissions vs. the Overall Press
Page 5 and 6: Flametube Combustor Emissions Reduc
Page 7 and 8: Fuel Flexible/Low Emissions Combust
Page 9 and 10: 75% Nox Reduction Injector Developm
Page 11: Time--> C 8 C 9 C 10 C 11 F-T Fuel
Page 15 and 16: ASCR Plenum Design and Fabrication
Page 17 and 18: Ultra-Lean-Burning Combustors Are M
Page 19 and 20: Long Term Goal for Active Combustio
Page 21 and 22: Active Combustion Control Combustio
Page 23 and 24: SiC Electronics Status • Building
Page 25 and 26: SiC Pressure Sensor Status • The
Page 27 and 28: High Temperature Combustor Liner Ch
Page 29 and 30: ERA CMC LINER - Subtasks 1. Liner m
Page 31 and 32: ERA CMC Liner Material Testing- Env
Page 33 and 34: High Temperature Piezoelectric Mate

Chi-Ming Lee Chief of Combustion Branch NASA Glenn Research ...

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