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Licensed Unlicensed Requires Authentication Published by De Gruyter September 1, 2008

Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor

  • Alok Sinha,
From the journal International Journal of Turbo and Jet Engines
https://doi.org/10.1515/TJJ.2008.25.3.145
Published Online: 2008-09

©2011 by Walter de Gruyter GmbH & Co.

From the journal
International Journal of Turbo and Jet Engines
International Journal of Turbo and Jet Engines
Volume 25 Issue 3

Journal and Issue

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
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