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dc.contributor.advisorIan A. Waitz.en_US
dc.contributor.authorSpindler, Phillip Michaelen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2007-12-07T16:11:06Z
dc.date.available2007-12-07T16:11:06Z
dc.date.copyright2007en_US
dc.date.issued2007en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/39710
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.en_US
dc.descriptionIncludes bibliographical references (leaves 83-86).en_US
dc.description.abstractThe Environmental Design Space (EDS) is a multi-disciplinary design tool used to explore trade-offs among aircraft fuel burn, emissions, and noise. This thesis uses multiple metrics to assess an EDS model of a Boeing 777 aircraft. Starting from a detailed description of the EDS framework, a description of EDS model creation is outlined. The aircraft and engine model is assessed by a comparison to an industry-developed model and changes to the EDS model are explored to improve the model's predictive ability. The model is assessed by sensitivity studies on the inputs, component performance maps, and constraints. An alternate method of applying additional constraints to EDS results is also investigated. Finally, the model uncertainty is quantified using Monte Carlo simulations. This includes a study where all the inputs are varied and a study which investigates the implications of model uncertainty on trade study results. The comparison to the industry model shows that optimization around three design points is required to develop a model of acceptable accuracy.en_US
dc.description.abstract(cont.) The input sensitivity study shows that there are only a few key drivers to the EDS model, but the direction of the trends with some of these variables is counterintuitive due to the typical practice constraint of holding the aircraft thrust to weight ratio constant. The constraint sensitivity study reveals there are only a handful of constraints implemented in EDS and the current method for applying additional constraints can increase the resultant errors due to the response surfaces generated. The uncertainty studies reveal the implications of attempting to correct cases which would otherwise fail and how fixes can skew results and increase uncertainty. Finally, the trade study uncertainty analysis shows that EDS is capable of answering questions with higher confidence than one would assume from the results of the input uncertainty study since the uncertainty due to variables which are not changing in a trade study are not significant.en_US
dc.description.statementofresponsibilityby Phillip Michael Spindler.en_US
dc.format.extent86 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleEnvironmental Design Space model assessmenten_US
dc.title.alternativeEDS model assessmenten_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc176895054en_US


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