Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/64018
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dc.contributor.authorLow, Yong Lin
dc.date.accessioned2015-05-22T02:48:05Z
dc.date.available2015-05-22T02:48:05Z
dc.date.copyright2015en_US
dc.date.issued2015
dc.identifier.urihttp://hdl.handle.net/10356/64018
dc.description.abstractThis project report attempted to simulate the flight of a Boeing 747-400 operating under Continuous Descent Operation procedures in an environment with a constant wind velocity. The descent profile was divided into 6 segments each with 2 possible descent modes, namely the Constant Flight Path Angle and Constant Rate of Descent modes, yielding 64 combinations. The 64 combinations were simulated under 2 headwind and 2 tailwind conditions, with speeds of 25 knots and 50 knots. Flight performance calculations were performed at intervals of one second. The simulations showed that a pure constant Flight Path Angle descent was the most fuel efficient, but the introduction of constant rate of descent segments at low altitudes cause only small negative impact on fuel consumption.en_US
dc.format.extent57 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Aeronautical engineering::Air navigationen_US
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aviationen_US
dc.titleContinuous descent operations in high throughput and constant wind environmenten_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorMao Jian Fengen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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