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Integrated Physics-based Modeling and Experiments for Improved Prediction of Combustion Dynamics in Low-Emission SystemsConcurrent simulation and experiment was undertaken to assess the ability of a hybrid RANS-LES model to predict combustion dynamics in a single-element lean direct-inject (LDI) combustor showing self-excited instabilities. High frequency pressure modes produced by Fourier and modal decomposition analysis were compared quantitatively, and trends with equivalence ratio and inlet temperature were compared qualitatively. High frequency OH PLIF and PIV measurements were also taken. Submodels for chemical kinetics and primary and secondary atomization were also tested against the measured behavior. For a point-wise comparison, the amplitudes matched within a factor of two. The dependence on equivalence ratio was matched. Preliminary results from simulation using an 18-reaction kinetics model indicated instability amplitudes closer to measurement. Analysis of the simulations suggested a band of modes around 1400 Hz were due to a vortex bubble breakdown and a band of modes around 6 kHz were due to a precessing vortex core hydrodynamic instability. The primary needs are directly coupled and validated ab initio models of the atomizer free surface flow and the primary atomization processes, and more detailed study of the coupling between the 3D swirling flow and the local thermoacoustics in the diverging venturi section.
Document ID
20180000406
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Anderson, William E.
(Purdue Univ. West Lafayette, IN, United States)
Lucht, Robert P.
(Purdue Univ. West Lafayette, IN, United States)
Mongia, Hukam
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
January 16, 2018
Publication Date
January 1, 2015
Subject Category
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN46249
Report Number: GRC-E-DAA-TN46249
Funding Number(s)
CONTRACT_GRANT: NNX11AI62A
WBS: WBS 432938.11.01.03.06.02.08
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
combustion
simulation
stability
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