Shroud Cooling with Blade Rotation Using Discrete Holes and an Upstream Slot
Author:
Affiliation:
1. Louisiana State University, Baton Rouge, Louisiana 70820
2. University of Memphis, Memphis, Tennessee 38152
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.T4803
Reference22 articles.
1. Three-Dimensional Flows in Axial Turbomachines
2. Flow Visualization in a Linear Turbine Cascade of High Performance Turbine Blades
3. Three-Dimensional Flow in a Low-Pressure Turbine Cascade at Its Design Condition
4. Controlling the Secondary Flow in a Turbine Cascade by Three-Dimensional Airfoil Design and Endwall Contouring
5. Secondary Flow Measurements in a Turbine Cascade With High Inlet Turbulence
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