Sensitivity of Turbine Efficiency and Flow Structures to Varying Purge Flow
Author:
Affiliation:
1. ETH Zurich, 8092 Zurich, Switzerland
2. University of Stuttgart, 70569 Stuttgart, Germany
3. MTU Aero Engines GmbH, 80995 Munich, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44646
Reference20 articles.
1. An Experimental Investigation of a Gas Turbine Disk Cooling System
2. Rim Sealing of Rotor–Stator Wheelspaces in the Absence of External Flow
3. Performance of Radial Clearance Rim Seals in Upstream and Downstream Rotor–Stator Wheelspaces
4. Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame
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