Two dimensional axisymmetric optimization of intermediate compressor duct

Visa enkel post
dc.contributor.authorHessman Tanman, Robert
dc.contributor.departmentChalmers tekniska högskola / Institutionen för mekanik och maritima vetenskapersv
dc.contributor.departmentChalmers University of Technology / Department of Mechanics and Maritime Sciencesen
dc.contributor.examinerXixto, Carlos
dc.contributor.supervisorJonaaon, Isak
dc.date.accessioned2024-11-18T12:37:18Z
dc.date.available2024-11-18T12:37:18Z
dc.date.issued2024
dc.date.submitted
dc.description.abstractThe civil aviation industry is a well established option for fast and secure intercontinental transport of people and freight. The continuous use of aerospace propulsion as a modern day means of transportation contributes to the emissions of harmful gases that in excess contributes to the decay of the environment. Engineers are continuously making progress in optimizing the gas turbine engines used for aerospace propulsion in order to reduce the fuel consumption. There has been great progress over the years since the gas turbines was first introduced in aerospace propulsion during the second world war. The first gas turbine engines on aircraft’s where very loud and not very efficient in terms of reliability, lifespan and fuel consumption. The initial application for these engines where on military aircraft’s as it would take sometime before it was adapted by civil aviation, replacing the piston propeller engines. The turbofan engine is currently widely used by civil aviation for its propulsive efficiency with a high bypass and pressure ratio. The progress made over the last two centuries has been greatly affected by the invention of commercial computational fluid dynamics software’s. Numeric optimizations can now be coupled with CFD software’s that allows for optimization of complete modules and parts of the engine. This method aids engineers in reducing the wight and optimizing the performance on a component basis of the turbofan engine in order to reduce the emissions of harmful greenhouse gases.
dc.identifier.coursecodeMMSX25
dc.identifier.urihttp://hdl.handle.net/20.500.12380/308991
dc.language.isoeng
dc.setspec.uppsokTechnology
dc.subjectICD
dc.subjectFluent
dc.subjectICEM
dc.subjectGenetic Algorithm (GA)
dc.subjectPython
dc.titleTwo dimensional axisymmetric optimization of intermediate compressor duct
dc.type.degreeExamensarbete på grundnivåsv
dc.type.uppsokM
local.programmeMaskinteknik 180 hp (högskoleingenjör)
Ladda ner
Original bundle
Visar 1 - 1 av 1
Bild (thumbnail)
Namn:
Optimization_of_Intermediate_Compressore_Duct.pdf
Storlek:
2.26 MB
Format:
Adobe Portable Document Format
Beskrivning:
Ladda ner
License bundle
Visar 1 - 1 av 1
Bild (thumbnail)
Namn:
license.txt
Storlek:
2.35 KB
Format:
Item-specific license agreed upon to submission
Beskrivning:
Ladda ner
Samling
Examensarbeten på grundnivå