Clemonson Premixed Combustors Subcontract with DoE - Esteban Gonzalez
GM Direction Injection
GE Taps
Pratt and Whitney Crossflow
NASA Active Control - Jacob Stenzler
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Name: Jacob Stenzler Position: Ph.D. Mechanical Engineering - Graduated 2004 Project Title: Fuel Distribution of Modulated Liquid Jets in Crossflow Project Sponsor: NASA |
The jet-in-crossflow configuration is a common injection configuration for Lean Premixed Prevaporized (LPP) and Lean Direct Injection (LDI) combustors. The objective of this project is to develop a model for active combustion control to characterize the fuel distribution of modulated liquid jets in crossflow. Diagnostic techniques include Mie scattering and stop-action photographs. The experiments are conducted in an atmospheric pressure facility at air velocities up to 110m/s and air temperatures up to 300°C using distilled water, acetone, and 4-heptanone as test liquids. Modulation is achieved using a standard automotive fuel injector at frequencies up to 100 Hz.
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Experimental setup for jet-in crossflow
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Stop action photographs showing the difference in atomization between an acetone spray (upper) and a water spray (lower) at the same crossflow velocity and momentum flux ratio [note: injection is steady-state] |
Recent Publications:
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Name: Esteban Gonzalez
Position: M.S. Mechanical Engineering - Graduated 2005 Project Title: Systematic measurements of global CH*, CO 2* and OH* chemiluminescence of turbulent fuel lean premixed flames Project Sponsor: DoE Subcontract with SCIES, Clemson University Future Project: Combustion instabilities in lean premixed gas turbine combustors. |
The measurement of heat release and pressure fluctuations is of great importance in the study of combustion instabilities in lean premixed gas turbine combustors. Usually a linear relationship between heat release and the intensity of chemiluminescence from species such as CH*, CO 2* and OH* is the base of the heat release measurements. The two objectives of this project are: 1) To experimentally investigate how parameters like combustor velocity, inlet temperature, equivalence ratio, swirl number, and fuel distribution affect the chemiluminecence intensity 2) Determine if the global chemiluminescence intensity from CH*, CO 2* and OH* will be a good indicator of heat release for a given range of the parameters mention above.
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Penn State Dump Combustor |
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