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Investigation of Unsteady Flow Phenomena in First Vane Caused by Combustor Flow With Swirl
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The flow at the combustor turbine interface of power generation gas turbines with can combustors is characterized by high and nonuniform turbulence levels, lengthscales, and residual swirl. These complexities have a ...
The Effect of Reaction on Compressor Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Reaction is the fundamental parameter by which the asymmetry of the velocity triangle of a stage is set. Little is understood about the effect that a reaction has on either the efficiency or the operating range of a ...
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