EconPapers    
Economics at your fingertips  
 

Generation and Propagation Characteristics of an Auto-Ignition Flame Kernel Caused by the Oblique Shock in a Supersonic Flow Regime

Wenxiong Xi, Mengyao Xu, Chaoyang Liu, Jian Liu and Bengt Sunden
Additional contact information
Wenxiong Xi: School of Aeronautics and Astronautics, Central South University, Changsha 410012, China
Mengyao Xu: School of Aeronautics and Astronautics, Central South University, Changsha 410012, China
Chaoyang Liu: College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410015, China
Jian Liu: School of Aeronautics and Astronautics, Central South University, Changsha 410012, China
Bengt Sunden: School of Aeronautics and Astronautics, Central South University, Changsha 410012, China

Energies, 2022, vol. 15, issue 9, 1-14

Abstract: The auto-ignition caused by oblique shocks was investigated experimentally in a supersonic flow regime, with the incoming flow at a Mach number of 2.5. The transient characteristics of the auto-ignition caused by shock evolvements were recorded with a schlieren photography system, and the initial flame kernel generation and subsequent propagation were recorded using a high-speed camera. The fuel mixing characteristics were captured using NPLS (nanoparticle-based planar laser scattering method). This work aimed to reveal the flame spread mechanism in a supersonic flow regime. The effects of airflow total temperature, fuel injection pressure, and cavity length in the process of auto-ignition and on the auto-ignitable boundary were investigated and analyzed. From this work, it was found that the initial occurrence of auto-ignition is first induced by oblique shocks and then propagated upstream to the recirculation region, to establish a sustained flame. The auto-ignition performance can be improved by increasing the injection pressure and airflow total temperature. In addition, a cavity with a long length has benefits in controlling the flame spread from the induced state to a sustained state. The low-speed recirculating region created in the cavity is beneficial for the flame spread, which has the function of flame-holding and prevents the flame from being blown away.

Keywords: auto-ignition; supersonic flow; initial flame kernel; oblique shock; recirculating region (search for similar items in EconPapers)
JEL-codes: Q Q0 Q4 Q40 Q41 Q42 Q43 Q47 Q48 Q49 (search for similar items in EconPapers)
Date: 2022
References: View references in EconPapers View complete reference list from CitEc
Citations:

Downloads: (external link)
https://www.mdpi.com/1996-1073/15/9/3356/pdf (application/pdf)
https://www.mdpi.com/1996-1073/15/9/3356/ (text/html)

Related works:
This item may be available elsewhere in EconPapers: Search for items with the same title.

Export reference: BibTeX RIS (EndNote, ProCite, RefMan) HTML/Text

Persistent link: https://EconPapers.repec.org/RePEc:gam:jeners:v:15:y:2022:i:9:p:3356-:d:808710

Access Statistics for this article

Energies is currently edited by Ms. Agatha Cao

More articles in Energies from MDPI
Bibliographic data for series maintained by MDPI Indexing Manager ().

 
Page updated 2025-03-19
Handle: RePEc:gam:jeners:v:15:y:2022:i:9:p:3356-:d:808710