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Effect of Pulsed Film Cooling on Leading Edge Film EffectivenessEI-GABRY, Lamyaa A; RIVIR, Richard B.Journal of turbomachinery. 2012, Vol 134, Num 4, issn 0889-504X, 041005.1-041005.6Article

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Suction-Side Gill Region Film Cooling: Effects of Hole Shape and Orientation on Adiabatic Effectiveness and Heat Transfer CoefficientCHAPPELL, Justin; LIGRANI, Phil; SREEKANTH, Sri et al.Journal of turbomachinery. 2010, Vol 132, Num 3, issn 0889-504X, 031022.1-031022.11Article

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Endwall Boundary Layer Development in an Engine Representative Four-Stage Low Pressure Turbine RigVERA, Maria; DE LA ROSA BLANCO, Elena; HODSON, Howard et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011017.1-011017.9Article

Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial Turbine-Part II: Unsteady Results and Boundary Layer BehaviorKÖNIG, Sven; STOFFEL, Bernd; TAHER SCHOBEIRI, M et al.Journal of turbomachinery. 2009, Vol 131, Num 2, issn 0889-504X, 021004.1-021004.8Article

Interstage Flow Interactions and Loss Generation in a Two-Stage Shrouded Axial TurbinePORRECA, L; KALFAS, A. I; ABHARI, R. S et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 11002.1-011002.12Article

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Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness on a Gas Turbine Blade TipMHETRAS, Shantanu; NARZARY, Diganta; ZHIHONG GAO et al.Journal of turbomachinery. 2008, Vol 130, Num 2, issn 0889-504X, 021002.1-021002.13Article

Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through Blockages With HolesLAU, S. C; CERVANTES, J; HAN, J. C et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031004.1-031004.9Article

Optimized Shroud Design for Axial Turbine Aerodynamic PerformancePORRECA, L; KALFAS, A. I; ABHARI, R. S et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031016.1-031016.12Article

The Influence of Shroud and Cavity Geometry on Turbine Performance: An Experimental and Computational Study-Part I: Shroud GeometryROSIC, Budimir; DENTON, John D; CURTIS, Eric M et al.Journal of turbomachinery. 2008, Vol 130, Num 4, issn 0889-504X, 041001.1-041001.10Article

Propulsion à plasma : vers de nouveaux concepts pour les missions du futur : Electrotechnique du futur = Plasma Propulsion : Towards New Concepts for Future MissionsGARRIGUES, Laurent; PEREZ-LUNA, Jaime; HAGELAAR, Gerjan J. M et al.REE. Revue de l'électricité et de l'électronique. 2008, Num 4, issn 1265-6534, 53-59, 68 [8 p.]Article

Advanced modeling of underplatform friction dampers for analysis of bladed disk vibrationPETROV, E. P; EWINS, D. J.Journal of turbomachinery. 2007, Vol 129, Num 1, pp 143-150, issn 0889-504X, 8 p.Article

Aeroelastic stability of welded-in-pair low pressure turbine rotor blades : A comparative study using linear methodsCORRAL, Roque; GALLARDO, Juan Manuel; VASCO, Carlos et al.Journal of turbomachinery. 2007, Vol 129, Num 1, pp 72-83, issn 0889-504X, 12 p.Article

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Gas turbine heat transfer : Ten remaining hot gas path challengesBUNKER, Ronald S.Journal of turbomachinery. 2007, Vol 129, Num 2, pp 193-201, issn 0889-504X, 9 p.Article

High-resolution film cooling effectiveness comparison of axial and compound angle holes on the suction side of a turbine vaneWAYE, Scot K; BOGARD, David G.Journal of turbomachinery. 2007, Vol 129, Num 2, pp 202-211, issn 0889-504X, 10 p.Article

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