OH PLIF Visualization of an Optically Accessible Rotating Detonation Combustor
Conference
·
· AIAA Propulsion and Energy 2019 Forum
- University of Michigan, Ann Arbor; University of Michigan
- University of Michigan, Ann Arbor
OH PLIF imaging has been successfully conducted within an optically accessible race- track shaped rotating detonation combustor. The OH PLIF images taken in this study corroborate the overall flow field structure reconstructed from previous OH* chemilumi- nescence studies conducted on the same combustor. However, the increased spatial and temporal resolution achieved with the OH PLIF technique allowed for the identification of previously unknown structures present in the detonation wave and its wake. These struc- tures appear as non-uniformities in the OH PLIF signal throughout the channel. Smaller scale structures range from variations in light intensity all the way to seemingly unburnt gas pockets passing through the detonation wave, suggesting non uniform reaction across the propagating detonation wave. Also present in the flow is a relatively large structure, consisting of a dark band surrounded by regions of higher OH intensity that trails the detonation wave. This band is hypothesized to be a result of the effect of secondary waves on the injection system and subsequent fill region composition stratification. Both of these flow structures represent potential avenues for performance loss through off-design mixing and heat release being uncoupled from the detonation wave.
- Research Organization:
- University of Michigan
- Sponsoring Organization:
- USDOE Office of Fossil Energy (FE)
- DOE Contract Number:
- FE0025315
- OSTI ID:
- 1808473
- Report Number(s):
- DOE-UMICH-FE0025315-016
- Conference Information:
- Journal Name: AIAA Propulsion and Energy 2019 Forum
- Country of Publication:
- United States
- Language:
- English
Similar Records
Study of Parasitic Combustion in an Optically Accessible Continuous Wave Rotating Detonation Engine
Mass flow rate effect on a rotating detonation combustor with an axial air injection
On the effects of reactant stratification and wall curvature in non-premixed rotating detonation combustors
Conference
·
Sun Jan 06 23:00:00 EST 2019
·
OSTI ID:1808460
Mass flow rate effect on a rotating detonation combustor with an axial air injection
Journal Article
·
Tue Feb 16 23:00:00 EST 2021
· Shock Waves
·
OSTI ID:1808471
On the effects of reactant stratification and wall curvature in non-premixed rotating detonation combustors
Journal Article
·
Tue Feb 15 23:00:00 EST 2022
· Combustion and Flame
·
OSTI ID:1976993