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Privacy-aware community infrastructureE. Poursaeidi, H. Ghaemi, M. Charmchi
Abstract
Rights: UNKNOWN · cc-by-nc-nd · Source: journal-auto-sync:external:CROSSREF_ISSN
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Rotordynamic forces due to turbine tip leakage: part I—blade scale effects
10.1115/1.2841179 · 1997
Rotordynamic forces due to turbine tip leakage: part II—radius scale effects and experimental verification
10.1115/1.2841180 · 1997
Dynamic characteristics of a flexible bladed-rotor with Coulomb damping due to tip-rub
10.1016/s0022-460x(03)00647-3 · 2004
10.1115/2000-gt-0390
10.1115/2000-gt-0390
10.1115/gt2008-50290
10.1115/gt2008-50290
Unresolved referenced work
Kept as external metadata until matched
Numerical simulation for effects of Reynolds numbers on tip leakage flows in turbine
2007
10.2514/6.2006-20
10.2514/6.2006-20
Tip clearance effects in a turbine rotor: part I—pressure field and loss
10.1115/1.1368365 · 2000
Tip clearance effects in a turbine rotor: part II—velocity field and flow physics
2000
Three-dimensional turbulent flow of the tip leakage vortex in an axial compressor rotor passage
2000
No additional external references are available.