"uuid","repository link","title","author","contributor","publication year","abstract","subject topic","language","publication type","publisher","isbn","issn","patent","patent status","bibliographic note","access restriction","embargo date","faculty","department","research group","programme","project","coordinates" "uuid:b7a76cb1-8dcc-47e1-8e6f-0b46b78f3f50","http://resolver.tudelft.nl/uuid:b7a76cb1-8dcc-47e1-8e6f-0b46b78f3f50","Ignition modeling in methane-oxygen rocket engines: Design and modeling of a methane-oxygen rocket engine igniter using reacting flows with computational fluid dynamics","Akkermans, Christ (TU Delft Aerospace Engineering)","Zandbergen, B.T.C. (mentor); Gill, E.K.A. (graduation committee); van Zuijlen, A.H. (graduation committee); Delft University of Technology (degree granting institution)","2017","The influence of using different chemistry model and different chemical kinetics schemes on modeling combustion inside a rocket engine igniter are investigated. An igniter for a LOX/CH4 rocket engine is designed and a CFD model is developed which is used to model the designed igniter. Verification and validation methods are discussed.