External Thrust Induced by High-Pressure Pulse Detonation System
- https://doi.org/10.2991/icmmita-15.2015.253How to use a DOI?
- Pulse detonation engine; compression ratio; detonation velocity.
This study investigated the reaction characteristics in a pulse detonation engine, including pressure, temperature, compression ratio, sonic velocity, and detonation velocity, using CEC code and STAR-CD. The former was used for the calculation of equilibrium states, whereas the latter was used for the simulation of reaction dynamics. A complete pulse detonation tube and measurement system were designed for these experiments with monitoring and recording performed using Lab VIEW. The ignition energy as well as detonation pressure and temperature were studied experimentally and the results were compared with numerical predictions. Our results provide useful insight into the design and performance of pulse detonation engines.
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Hsin-Po Chen AU - Chia-Nan Wang AU - Ming-Hsien Hsueh PY - 2015/11 DA - 2015/11 TI - External Thrust Induced by High-Pressure Pulse Detonation System BT - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 1364 EP - 1370 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-15.2015.253 DO - https://doi.org/10.2991/icmmita-15.2015.253 ID - Chen2015/11 ER -