Combustion instability modeling and analysis
Description:
It is well known that the two key elements for achieving low emissions and high performance in a gas turbine combustor are to simultaneously establish (1) a lean combustion zone for maintaining low NO{sub x} emissions and (2) rapid mixing for good ignition and flame stability. However, these requirements, when coupled with the short combustor lengths used to limit the residence time for NO formation typical of advanced gas turbine combustors, can lead to problems regarding unburned hydrocarbons…
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Date:
December 31, 1995
Creator:
Santoro, R.J.; Yang, V.; Santavicca, D.A. & Sheppard, E.J.
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Partner:
UNT Libraries Government Documents Department