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Mistuning Analyses of a Bladed Disk: Pole-Zero and Modal Approaches
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Alok Sinha,
Published/Copyright:
March 1, 2010
Published Online: 2010-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- The New Era of Stealth, Tailless, Vectored Aircraft. A 2010 Review on Current & Future Designs and Applications of Manned and Unmanned, Super-Agile and Safest Military v. Civil Jets
- Mistuning Analyses of a Bladed Disk: Pole-Zero and Modal Approaches
- Experimental Study on Flow and Heat Transfer in Circular Small-scale Channels for Aeroengines
- Theoretical Analysis of Rotating Stall Under Static Inflow Distortion Including Effect of Tip Injection
- Cold Flow Studies on the Effect of Injector Locations in a Directly Injected Cavity Based Combustor
- Kerosene Fuelled Tubular Type Combustion Chamber Gas Turbine Engine: Design Methodology and Numerical Investigations
- Development of On-line Performance Diagnostic Program of a Helicopter Propulsion System
Articles in the same Issue
- CONTENTS
- The New Era of Stealth, Tailless, Vectored Aircraft. A 2010 Review on Current & Future Designs and Applications of Manned and Unmanned, Super-Agile and Safest Military v. Civil Jets
- Mistuning Analyses of a Bladed Disk: Pole-Zero and Modal Approaches
- Experimental Study on Flow and Heat Transfer in Circular Small-scale Channels for Aeroengines
- Theoretical Analysis of Rotating Stall Under Static Inflow Distortion Including Effect of Tip Injection
- Cold Flow Studies on the Effect of Injector Locations in a Directly Injected Cavity Based Combustor
- Kerosene Fuelled Tubular Type Combustion Chamber Gas Turbine Engine: Design Methodology and Numerical Investigations
- Development of On-line Performance Diagnostic Program of a Helicopter Propulsion System
