Tip-Shroud Cutbacks in a Low-Pressure Gas Turbine Stage
Author:
Affiliation:
1. Swiss Federal Institute of Technology, 8092 Zurich, Switzerland
2. Aristotle University of Thessaloniki, 541 24 Thessaloniki, Greece
3. MTU Aero Engines AG, 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.B35522
Reference33 articles.
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2. KurzkeJ. “Fundamental Differences Between Conventional and Geared Turbofans,” Proceedings of the ASME Turbo Expo, American Soc. of Mechanical Engineers Paper GT2009-59745, 2009.
3. Geared Fan Engine Systems-Their Advantages and Potential Reliability
4. Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage
5. SelicT.LenganiD.MarnA.HeitmeirF. “Aerodynamic Effects of an Unshrouded Low Pressure Turbine on a Low Aspect Ratio Exit Guide Vane,” Proceedings of the ASME Turbo Expo, American Soc. of Mechanical Engineers Paper GT2012-68981, 2012.
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