Analysis of Combustion Characteristics of Can-Type and Annular-Type Combustion Chamber
Abstract High performance is always desired for the propulsion system and the assortment of a better combustion type is also a vital part of the propulsion system. The analysis of different designs of combustion chambers and comparison of their combustion characteristics. In this paper, the assessment of Can-type and Annular-type combustion chambers and the design developed with SOLIDWORKS software and analysis done with ANSYS FLUENT. The systematic and translucent method approaches reduce the design complexity and time. The combustion with turbulence interface was examined to analyze with precision results, and the analysis specified that the nowadays experiment depends on the behavior of gas exit pressure, temperature, and velocity. Parametric analysis is used to acquire the sizing of the combustion chamber.
Authors
- M. R. S. Satyanarayana
- D. Smitha
- Sachin Kumar Srivastava (ORCID: https://orcid.org/0000-0003-1711-1551)
Institutions
- Uttaranchal University (IN)
- GITAM University (IN)
Publication Details
- Journal
- Journal of Physics Conference Series
- Published
- 2024-10-01
- DOI
- https://doi.org/10.1088/1742-6596/2856/1/012004
- Primary Topic
- Rocket and propulsion systems research
- Type
- article
- Field-Weighted Citation Impact
- 0.00