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Fuel Burn and Emissions Reduction Potential of Low Power/Low Drag Approaches

Author(s)
Dumont, Jean-Marie; Hansman, Robert J., Jr.; Reynolds, Thomas G.; Hansman, Robert J., Jr.; Hansman, Robert J., Jr.
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Abstract
Changing aircraft operational procedures is one strategy that can be used to reduce fuel burn and mitigate environmental impacts of aviation in relatively short timeframes with existing aircraft types. This study quantifies the fuel burn and emissions reduction potential of delayed deceleration approaches, where the aircraft is kept fast and in clean aerodynamic configuration for as long as possible during the approach phase of flight. This reduces the drag and thrust requirements and these procedures are therefore called Low Power/Low Drag approaches. Operational data is used to characterize approach profiles, together with their fuel burn and emissions properties correlated to airspeed and configuration for a selection of aircraft types. Aircraft that were observed to decelerate and configure flaps later in the approach had 30-40% lower fuel burn and carbon dioxide emissions below 10,000 ft compared to those that did not. Estimates of US system-wide fuel burn and emissions reduction potential from Low Power/Low Drag approaches are provided: if only 1% of the total operations used these approaches, savings across all operators would amount to 2.9 million US gallons ($5.8-11.6 million at $2-4/US gallon) of fuel and 28,000 metric tons of carbon dioxide emissions per year. A discussion is provided on the implementation barriers which need to be addressed if benefits are to be realized.
Date issued
2011-09
URI
http://hdl.handle.net/1721.1/96977
Department
Lincoln Laboratory; Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Journal
Proceedings of the 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
Publisher
American Institute of Aeronautics and Astronautics
Citation
Dumont, Jean-Marie, Tom Reynolds, and R John Hansman. “Fuel Burn and Emissions Reduction Potential of Low Power/Low Drag Approaches.” 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference (September 20, 2011).
Version: Author's final manuscript
ISBN
978-1-60086-941-9

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