Various research topics on Combustion/Propulsion/Energy Systems
Thursday, September 29th, 2011Thursday September 29, 2011 4:00-5:00 p.m.
ME-EM building, Room 112
Professor Jong Guen Lee
Ohio Research Scholar in the School of Aerospace Systems at the University of Cincinnati.
The seminar will give a brief summary on various research topics in combustion/propulsion/energy areas which include the combustion dynamics in advanced gas turbine engines, the combustion of nano-energetics and the development of advanced propulsion/energy systems.
Combustion instabilities pose significant operational problems for gas turbine engines. Most of these instabilities involve a resonant coupling between the combustion-generated heat release rate and acoustic waves in combustor. One important factor required to understand combustion instabilities is to know how the flame responses to acoustic perturbations. This, so-called flame transfer function, has been determined for various nozzles. Some of the results will be presented and the phenomenology of flame response to inlet velocity and fuel modulation will be discussed.
Thermite reactions with nanoscale particles have attracted much study due to their high flame temperatures and combustion velocities. However, the mechanism by which the reaction propagates is not well understood. The fuel and oxidizer particle sizes of Al/CuO and Al/Mo03 thermites were varied between the nanometer and micrometer scale, are presented to gain further insight into the factors governing their rate of propagation. Critical properties, including linear propagation rates, dynamic pressure, spectral emission and burning temperature, were measured and compared to address the flame propagation mechanism.
Currently, there is a high demand for smaller satellites and thus smaller load areas, which in turn require better onboard power sources. SOFCs (Solid Oxide Fuel Cells) can incorporate an electric generator into a system that will run off of the gases created during combustion from the onboard thrusters of satellite systems. The SOFC can generate power from the exhaust gases created by the thrusters and store the electric output into a super capacitor to use at a later time. This eliminates the need for an onboard battery or other types of electric storage units, lowering the overall weight and size. A unique concept developed to achieve this and its feasibility will be discussed.
