Show simple item record

dc.contributor.advisorSteven R. H. Barrett.en_US
dc.contributor.authorBrink, Lukas Frederik Jakob.en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2021-01-06T18:33:03Z
dc.date.available2021-01-06T18:33:03Z
dc.date.copyright2020en_US
dc.date.issued2020en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/129181
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, September, 2020en_US
dc.descriptionCataloged from student-submitted PDF of thesis. In title on title page, x̳ appears as subscript x.en_US
dc.descriptionIncludes bibliographical references (pages 103-114).en_US
dc.description.abstractAircraft NO[subscript x], CO and soot emissions contribute to climate change and lead to negative air quality impacts. With the aim of quantifying the effects of fuel composition on NO[subscript x], CO and soot emissions, a combustor model named Pycaso is developed. The combustor model consists of a 0D/1D reactor network, coupled with a soot model. The model predicts NO[subscript x], CO and soot emissions at sea level conditions for a CFM56-7B engine using conventional jet fuel. The model matches existing methods to predict cruise NO[subscript x] emissions within 5% and cruise CO emissions within 30%. It is shown that the volume -- and thus time -- over which secondary air is mixed with the fuel-air mixture in the combustor is the most important factor in determining the magnitudes of the modeled emissions. The sensitivity of modeled NO[subscript x] and CO emissions to thrust at thrust settings below 15% is shown to be the consequence of "cold" unburned fuel entering the secondary zone of the combustor. The model is used to assess two possible emission mitigation solutions: removing naphthalene from jet fuel and replacing conventional jet fuel with 50:50 biofuel blends. The removal of naphthalene through hydrotreating is found to lead to mean reductions in soot emissions of 15% [12%-20%] for mass and 9% [5%-19%] for number. The range captures variations in engine operating conditions, soot model configurations and compositions of the baseline jet fuel. Similarly, the removal of naphthalene through extractive distillation reduces soot mass emissions by 32% [29%-48%] and number emissions by 23% [14%-45%]. The mean reductions associated with using 50:50 biofuel blends are 43% [34%-59%] for soot mass and 35% [14%-45%] for soot number. Using biofuel blends is also predicted to result in a reduction in NO[subscript x] emissions of 5% [4%-7%] and a 3% [2%-4%] decrease in CO emissions.en_US
dc.description.statementofresponsibilityby Lukas Frederik Jakob Brink.en_US
dc.format.extent114 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleModeling the impact of fuel composition on aircraft engine NOx̳, CO and soot emissionsen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc1227278199en_US
dc.description.collectionS.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2021-01-06T18:33:01Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentAeroen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record