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Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
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H. Pathak,
Published/Copyright:
September 1, 2008
Published Online: 2008-09
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
- Active and Passive Flow Control in a Turbine Cascade
- Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
- Turbomachine Shrouded Rotor Blade Forced Response Analysis
- Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
- Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
- Performance Improvement of Gas Turbine Cycles
- Characteristics of Supersonic Impinging Moist Air Jets
Articles in the same Issue
- CONTENTS
- Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
- Active and Passive Flow Control in a Turbine Cascade
- Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
- Turbomachine Shrouded Rotor Blade Forced Response Analysis
- Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
- Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
- Performance Improvement of Gas Turbine Cycles
- Characteristics of Supersonic Impinging Moist Air Jets
