Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/115422
DC FieldValue
dc.titleExperimental investigations on DDT enhancements by shchelkin spirals in a PDE
dc.contributor.authorNew, T.H.
dc.contributor.authorPanicked, P.K.
dc.contributor.authorLu, F.K.
dc.contributor.authorTsai, H.M.
dc.date.accessioned2014-12-12T07:15:25Z
dc.date.available2014-12-12T07:15:25Z
dc.date.issued2006
dc.identifier.citationNew, T.H.,Panicked, P.K.,Lu, F.K.,Tsai, H.M. (2006). Experimental investigations on DDT enhancements by shchelkin spirals in a PDE. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting 9 : 6674-6683. ScholarBank@NUS Repository.
dc.identifier.isbn1563478072
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/115422
dc.description.abstractAn experimental investigation was carried out on a multi-cycle pulsed detonation engine, running on a propane-oxygen mixture using a rotary-valve injection system and a low energy ignition source, to study the effectiveness of Shchelkin spiral parameters on the deflagration-to-detonation transition (DDT) phenomenon. Various configurations were tested using spirals with blockage-ratios ranging from 34.7 to 55.6 % and spiral length to diameter ratio of 12.5 and 24.4. The results showed that only spirals with the highest blockage-ratio were able to achieve successful and sustained DDT in the shorter length configuration. However, further studies revealed that lower blockage-ratio spirals were able to achieve successful DDT when their lengths were 24.4 times that of the detonation tube diameter with corresponding higher levels of peak thrust production observed. Lastly, practical operating issues regarding the use of Shchelkin spirals are discussed in this paper.
dc.sourceScopus
dc.typeConference Paper
dc.contributor.departmentTEMASEK LABORATORIES
dc.description.sourcetitleCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
dc.description.volume9
dc.description.page6674-6683
dc.identifier.isiutNOT_IN_WOS
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