AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 ...

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Fuel Burn Baselines and Results PFEI for 50 Best Existing Aircraft within Global Fleet Computed using Piano-X software D8.5 H3.2 8
D Series Configuration is a Key Innovation D8 configuration 2035 Engine Technology Airframe materials/processes Natural laminar flow on bottom wing Airframe load reduction Approach operations LDI combustor % Fuel burn reduction relative to baseline % LT NOx reduction relative to CAEP6 %0 0 %10 -10 %20 -20 %30 -30 %40 -40 %50 Balanced Field Length for all designs = 5000 feet Fuel burn Noise LTO NOx -50 EPNdB Noise reduction relative to Stage 4 %60 -60 9
Page 1 and 2: AIRCRAFT AND TECHNOLOGY CONCEPTS FO
Page 3 and 4: Project Enabled by University-Indus
Page 5 and 6: Three Major Results from N+3 Progra
Page 7: D and H Series Fuel Burn for Differ
Page 11 and 12: D8 - Double Bubble Configuration wi
Page 13 and 14: D8.5 Engine Technology Overview Hig
Page 15 and 16: Fuel burn evolution from B737-800 t
Page 17: Noise evolution from B737-800 to D8
Page 20 and 21: Improved Load/Unload Time and Airpo
Page 22 and 23: Summary • Established documented

AIRCRAFT AND TECHNOLOGY CONCEPTS FOR AN N+3 ...

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