Combustion Fundamentals Group
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Approach Experiments are performed in an
optically-accessible catalytic combustion chamber (see Fig. 1). The flow
in the catalytic combustor can be either laminar or turbulent. Advanced laser‑based
spectroscopic techniques are applied, in cooperation with the Combustion
Diagnostics group, to map the species and temperature profiles along the
streamwise plane of symmetry (see Fig. 2). In turbulent catalytic
combustion, PIV is used to map the velocity field. Two‑dimensional
steady and transient elliptic fluid mechanical codes have been in‑house developed,
which are capable of treating detailed heterogeneous and homogeneous chemical
reaction schemes and all relevant heat transfer mechanism in the solid. Analytical
ignition criteria based on matched activation energy asymptotics are also
derived.
Fig. 1: (a) Schematic of the high-pressure
catalytic combustion test rig. The steam generator unit is used for simulating
exhaust gas recycle. (b) Photograph of the test rig (top) and detail of the
reactor under operation as seen through the side quartz windows.
Fig. 2: Optical setup for spontaneous Raman and
laser induced fluorescence (LIF) measurements. Recent studies
1) Fuel-lean catalytic combustion of methane/air
mixtures over platinum
Fig. 3: Comparison between measured (a) and
predicted (b, c, d) maps of the OH radical in high‑pressure catalytic combustion
of methane over platinum. The green arrows indicate the onset of homogeneous
ignition. The predictions refer to different homogeneous chemical reaction
mechanisms. 2)
Fuel-lean catalytic combustion of hydrogen/air
mixtures over platinum
Fig. 4: Left graph: Comparison between measured (a) and predicted (b, c, d) maps of
the OH radical in atmospheric pressure catalytic combustion of hydrogen over
platinum. The predictions refer to different homogeneous chemical reaction
mechanisms. Right
graph: Comparison between measured (symbols) and predicted (lines) transverse
profiles of species mass fractions and temperature.
Fig. 5: (a) PIV‑measured instantaneous vorticity
maps in: (I) a non‑reacting isothermal channel flow with inlet Reynolds number
of 30,000 and (II) in catalytic combustion flow with the same incoming Reynolds
number. (b)
Domains of flow laminarization in channel‑flow catalytic combustion in terms of
inlet Reynolds number, wall temperature, and inlet turbulence intensity. 4) Analytical ignition criteria in channel‑flow
CST
Fig. 6: Left: analytical homogeneous ignition
criterion in channel‑flow CST. Right: comparison of analytical and numerical
solutions. |
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