Back to Search
Start Over
Research on the influence of different obstacle structures on the energy distribution characteristics of pulse detonation gas
- Source :
- Thermal Science, Vol 26, Iss 1 Part B, Pp 759-769 (2022)
- Publication Year :
- 2022
- Publisher :
- National Library of Serbia, 2022.
-
Abstract
- In order to improve the gas energy conversion efficiency at the outlet of the pulse detonation combustor, numerical calculation methods were used to study the influence of three different cross-section obstacle structures of square, circle and trapezoid on the distribution characteristics of gas pressure potential energy, kinetic energy and internal energy in a single cycle at the outlet of pulse detonation combustor. The results show that: the expansion of pulse detonation gas mainly includes three stages: primary expansion, secondary expansion, and over-expansion. Gas pressure potential energy, kinetic energy and internal energy increase during the primary and secondary expansion stages, and decrease during the over-expansion stage; Pulse detonation combustor with trapezoidal cross-section obstacle structure has the smallest proportion of gas energy at the outlet of the combustor during the over-expansion stage and the highest proportion during the secondary expansion stage; compared with square and circle cross-section obstacle structures, the gas energy distribution at the outlet of the pulse detonation combustor with trapezoidal cross-section obstacle structure is the easiest for turbomachinery to convert the gas energy.
- Subjects :
- Materials science
Internal energy
Renewable Energy, Sustainability and the Environment
Energy conversion efficiency
Detonation
detonation wave
obstacle structure
Mechanics
Kinetic energy
Potential energy
Pulse (physics)
expansion
Turbomachinery
TJ1-1570
Combustor
Mechanical engineering and machinery
pulse detonation combustor
combustion
energy
Subjects
Details
- ISSN :
- 23347163 and 03549836
- Volume :
- 26
- Database :
- OpenAIRE
- Journal :
- Thermal Science
- Accession number :
- edsair.doi.dedup.....6ce6680b3f7f897e389af71b3382697b