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Vortex/flame interaction is an important mechanism for unsteady combustion in a swirl combustion system. Technology of low emission stirred swirl(Te LESS), which is characterized with stratified swirl flow, has been developed in Beihang University to reduce NOXemission. However,large-scale flow structure would be induced in strong swirl flow. Experiments and computational fluid dynamics(CFD) simulation were carried out to investigate the unsteady flow feature and its mechanism in Te LESS combustor. Hotwire was firstly applied to testing the unsteady flow feature and a distinct mode with 2244 Hz oscillation frequency occurred at the pilot swirl outlet.The flow mode amplitude decayed convectively. Large eddy simulation(LES) was then applied to predicting this flow mode and know about its mechanism. The deviation of mode prediction compared with hotwire test was 0.8%. The spiral isobaric structure in pilot flow passage indicates that precessing vortex core(PVC) existed. The velocity spectrum and phase lag analysis suggest that the periodic movement at the pilot outlet was dominated by precessing movement. Negative tangential momentum gradient reflects that the swirl flow was unstable. Another phenomenon was found out that the PVC movement was intermittently rotated along the symmetric axis.
Vortex / flame interaction is an important mechanism for unsteady combustion in a swirl combustion system. Technology of low emission stirred swirl (Te LESS), which is characterized with stratified swirl flow, has been developed in Beihang University to reduce NOXemission. However, large- scale flow structure would be induced in strong swirl flow. Experiments and computational fluid dynamics (CFD) simulation were carried out to investigate the unsteady flow feature and its mechanism in Te LESS combustor. Hotwire was first applied to testing the unsteady flow feature and a distinct mode with 2244 Hz oscillation frequency occurred at the pilot swirl outlet. The flow mode amplitude decayed convectively. Large eddy simulation (LES) was then applied to predicting this flow mode and know about its mechanism. The deviation of mode prediction compared with hotwire test was 0.8%. The spiral isobaric structure in pilot flow passage says that precessing vortex core (PVC) existed. The velocity spect rum and phase lag analysis suggest that the periodic movement at the pilot outlet was dominated by precessing movement. Negative tangential momentum gradient competent that the swirl flow was unstable unstable. Another phenomenon was found out that the PVC movement was intermittently rotated along the symmetric axis.