| Flame tomography by tunable infrared diode laser absorption
A tunable infrared diode laser was used for absorption tomography in an axisymmetric atmospheric pressure flat-flame burner. Profiles of temperature and CO2 mole fraction were measured simultaneously. Experiments were conducted in methane-air flames with stoichiometries ranging from lean to rich. Absorption measurements were made just short of the R-branch band head at 4.17 µm to minimize interferences with other species, while providing good temperature and concentration sensitivity at flame conditions. The tomographic reconstructions were successful when spectra were taken just short of the nu-3 band head. Spectra that include the band head show large line shifts of the R(110) R(122) lines in flames. The shift varies rapidly with rotational quantum number, but is not observed in measurements of pure CO2 in a cell. The flame measurements also showed an anomalously intense absorption in the region of the R(116) R(124) transitions. The cause of this anomaly has not been determined and requires further investigation. |
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| High Repetition Rate Raman Facility for Turbulent Combustion
with Guanhua Wang and Prof. Noel T. Clemens We are developing a high power (~100 W) Raman scatterring instrument that will operate at 10-15 kHz in order to obtain simultaneous measurements of several major species (fuel, oxidiser, products) and temperature at rates two to three orders of magnistude faster than conventional Raman systems. |
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| Plasma Ignition of Solid Propellants
with Mike Ryan and Prof. Noel T. Clemens A study is being conducted of plasma-induced ignition of solid propellants. Work to date has included the characterization of a pulsed plasma jet resulting from a capillary discharge. An image of the visible emission of the plasma jet, as captured by a fast shuttering intensified camera, is shown at right. Planar laser induced fluorecence image of copper atom in a capillary discharge |
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| Adaptive Hybrid Continuum and Rarefied Flowfield Computation
With Roberto Roveda (now with Intel) and Prof. David Goldstein Flows with significant continuum and rarefied zones
are important in a number of practical situations. The application of immediate
interest is the impingement of plumes on the solar panels of the International
Space Station during Space Shuttle docking maneuvers. We use Direct Simulation
Monte Carlo (DSMC) in the regions of significant gradients and a discrete
velocity method in the equilibrium zone. The two regions are coupled and
the boundaries are continuously adapted to track moving shocks, expansion
waves, boundary layers, etc.
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DSMC Simulations of Volcanic Flows on Io With Ju Zhang and Prof. David Goldstein Io has a tenuous atmosphere that arises from volcanic activity. We model the rarefied plumes on Io and compute radiation from the plumes for comparison to observations that can be made from ground and space-based telescopes. Plume features include a canopy shock, supersonic gravity driven flows, and regions of extreme non-equilibrium where the classical thermodynamic or kineitc definitions of temperature are misleading. Io was studied by NASA's Galileo probe which took some great pictures and movies. |
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| Numerical Solution of the Extended Bolzmann Equation
This work is an extension of the Delta-Epsilon method (Z. Tan and P. L. Varghese, J. Computational Physics 110, pp. 327-340, 1994) in which one uses a discrete velocity approximation in the infinite velocity space, but considers only those distribution function points which that exceed a threshold value. The distribution function points may occur anywhere in the infinite discrete velocity space and are not constrained to a pre-specified region. A fourth-order finite difference is used for the convection terms. A Monte Carlo-like method is applied to the discrete velocity model of the collision integral. The effort of the method is proportional to the number of discrete points. Currently the method is being extended to include rotational and vibrational energy modes of molecules and gas mixtures |
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| Unsteady flow computations by the Delta-Epsilon method.The link at right goes to an animation of the developing density field for rarefied flow over a flat plate showing the development of a shock at the leading edge and expansion at the trailing edge. You may have to click on the image to start the animation. | Link to density field animation |
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