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Effect of Nozzle Guide Vane Lean Under Influence of Inlet Temperature Traverse
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: One of the most widely studied parameters in turbine blade shaping is blade lean, i.e., the tangential displacement of spanwise sections. However, there is a lack of published research that investigates the effect of blade ...
Analysis of Radial Migration of Hot Streak in Swirling Flow Through High Pressure Turbine Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The high pressure (HP) turbine is subject to inlet flow nonuniformities resulting from the combustor. A leanburn combustor tends to combine temperature variations with strong swirl and, although considerable research efforts ...
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