Research graph
References from Effects of temperature gradient on compressor casing in an industrial gas turbine. Local targets link to admitted publications; unresolved targets remain external evidence.
Rotordynamic forces due to turbine tip leakage: part I—blade scale effects
10.1115/1.2841179 · 1997 · External reference
Rotordynamic forces due to turbine tip leakage: part II—radius scale effects and experimental verification
10.1115/1.2841180 · 1997 · External reference
Dynamic characteristics of a flexible bladed-rotor with Coulomb damping due to tip-rub
10.1016/s0022-460x(03)00647-3 · 2004 · External reference
10.1115/2000-gt-0390
10.1115/2000-gt-0390 · External reference
10.1115/gt2008-50290
10.1115/gt2008-50290 · External reference
Unresolved reference
External reference
Numerical simulation for effects of Reynolds numbers on tip leakage flows in turbine
2007 · External reference
10.2514/6.2006-20
10.2514/6.2006-20 · External reference
Tip clearance effects in a turbine rotor: part I—pressure field and loss
10.1115/1.1368365 · 2000 · External reference
Tip clearance effects in a turbine rotor: part II—velocity field and flow physics
2000 · External reference
Three-dimensional turbulent flow of the tip leakage vortex in an axial compressor rotor passage
2000 · External reference
