experimental investigation of a reacting transverse jet in a high pressure oscillating vitiated crossflow

Staged combustion is one design approach in a gas turbine engine to reduce pollutant emission levels. In axially staged combustion, portions of the air and fuel are injected downstream of a lean premixed low NOx primary combustion zone. The gas residence time at elevated temperatures is decreased resulting in lower thermal NOx, and the reduced oxygen and high temperature vitiated primary zone flow further help to reduce pollutant emissions and quickly complete combustion.

Name thesis:degree_name

Doctor of Philosophy (PhD)

Level thesis:degree_level

Dissertation

Discipline thesis:degree_discipline

Aeronautics and Astronautics

Year

2015

Author dc:creator

• Fugger, Christopher Allen

Contributors dc:contributor

• William E Anderson
• Steve D Heister
• Robert P Lucht
• Enrique E Portillo Bilbao

• acoustics
• combustion
• dump combustor
• oscillating crossflow
• reacting jet in crossflow
• transverse jet

Repository record dc:identifier

https://docs.lib.purdue.edu/open_access_dissertations/1352

OAI identifier oai:identifier

oai:docs.lib.purdue.edu:open_access_dissertations-2568