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An Investigation of Simulated Flight Fatigue of TC4 Titanium Alloy Gas Turbine Blading
-
Z.L. Zhuang,
Published/Copyright:
March 1, 1993
Published Online: 1993-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Complete Thrust Vectoring Flight Control for Future Civil Jets, F-22 Superiority Fighter and Cruise Missiles. Part I: Vectored F-22, F-16 and F-15
- Aerodynamic Design and Investigation of a High-Loaded Turbine
- Propulsion System Flight Test Analysis Using Modeling Techniques
- Off-Design Performance Prediction for Radial-Flow Impellers
- Flow Visualization in a Circular-to-Rectangular Transition Duct
- An Investigation of Simulated Flight Fatigue of TC4 Titanium Alloy Gas Turbine Blading
Articles in the same Issue
- CONTENTS
- Complete Thrust Vectoring Flight Control for Future Civil Jets, F-22 Superiority Fighter and Cruise Missiles. Part I: Vectored F-22, F-16 and F-15
- Aerodynamic Design and Investigation of a High-Loaded Turbine
- Propulsion System Flight Test Analysis Using Modeling Techniques
- Off-Design Performance Prediction for Radial-Flow Impellers
- Flow Visualization in a Circular-to-Rectangular Transition Duct
- An Investigation of Simulated Flight Fatigue of TC4 Titanium Alloy Gas Turbine Blading
