Please use this identifier to cite or link to this item:
|Title:||Deflagration to detonation transition by hybrid obstacles in pulse detonation engines||Authors:||Li, J.
|Issue Date:||2013||Citation:||Li, J.,Teo, C.J.,Lim, K.S.,Wen, C.,Khoo, B.C. (2013). Deflagration to detonation transition by hybrid obstacles in pulse detonation engines. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. ScholarBank@NUS Repository.||Abstract:||A hybrid DDT enhancement device comprising obstacles of orifice plates and vortex generators is investigated to achieve reliable and repeatable detonations in Pulse Detonation Engines. The vortex generator is capable of yielding homogenous mixing while detonation transition can be achieved by it. The experimental results of deflagration to detonation transition process by a series of designed obstacles are reported. All experiments were carried out using a valveless PDE operated for multiple cycles using stoichiometric ethylene/air mixtures. The results show that initiation of DDT starting within vortex generator can enhance DDT process and achieve a strong overdriven detonation. In addition, during the transition stage, the onset of detonation can occur inside the vortex generator; while it generally takes place after the obstacles terminated. It is realized that effectiveness of the DDT enhancement device depends on the operation frequency. A hybrid obstacle of 0.4m orifice plates connecting 0.5m vortex generator can achieve reliable and repeatable transition within 15 L/D DDT run-up distance.||Source Title:||49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference||URI:||http://scholarbank.nus.edu.sg/handle/10635/73308||ISBN:||9781624102226|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Jun 21, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.