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Secondary Flow Loss Reduction Through Blowing for a High-Lift Front-Loaded Low Pressure Turbine CascadeBENTON, Stuart I; BONS, Jeffrey P; SONDERGAARD, Rolf et al.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021020.1-021020.8Article

Investigation of a Bird Strike Incident of a Military Gas Turbine EngineMISHRA, R. K; AHMED, S. I; SRINIVASAN, K et al.Journal of failure analysis and prevention. 2013, Vol 13, Num 6, pp 666-672, issn 1547-7029, 7 p.Article

Failure Analysis and Repair of a Catastrophically Damaged Gas Turbine Compressor Disk Using SEM Technique and CFD AnalysisTORABI, A. R; BAYATI, M.Journal of failure analysis and prevention. 2012, Vol 12, Num 4, pp 391-401, issn 1547-7029, 11 p.Article

LAS MÁQUINAS DE VAPOR EN LA OBTENCIÓN DEL AZÚCAR DE CAÑA EN ESPAÑA: ANÁLISIS COMPARATIVO = THE STEAM ENGINES IN SUGARCANE PRODUCTION IN SPAIN: COMPARATIVE ANALYSISROJAS-SOLA, José Ignacio; URENA-MARIN, José Ramon.Dyna (Medellín). 2012, Vol 171, pp 183-190, issn 0012-7353, 8 p.Article

A scaling method for combustion stability rating of coaxial gas-liquid injectors in a subscale chamberCHAE HOON SOHN; YOUNG JUN KIM; KIM, Young-Mog et al.Journal of mechanical science and technology. 2012, Vol 26, Num 11, pp 3691-3699, issn 1738-494X, 9 p.Article

A Film-Cooling Correlation for Shaped Holes on a Flat-Plate SurfaceCOLBAN, Will F; THOLE, Karen A; BOGARD, David et al.Journal of turbomachinery. 2011, Vol 133, Num 1, issn 0889-504X, 011002.1-011002.11Article

Effects of Multiblocking and Axial Gap Distance on Performance of Partial Admission Turbines: A Numerical AnalysisBAAGHERZADEH, Narmin; HUSHMANDI; FRANSSON, Torsten H et al.Journal of turbomachinery. 2011, Vol 133, Num 3, issn 0889-504X, 031028.1-031028.9Article

Experimental Measurements of Gas Turbine Flow Capacity Using a Novel Transient TechniquePOVEY, T; SHARPE, M; RAWLINSON, A et al.Journal of turbomachinery. 2011, Vol 133, Num 1, issn 0889-504X, 011005.1-011005.15Article

Experimental Simulation of a Film Cooled Turbine Blade Leading Edge Including Thermal Barrier Coating EffectsMAIKELL, Jonathan; BOGARD, David; PIGGUSH, Justin et al.Journal of turbomachinery. 2011, Vol 133, Num 1, issn 0889-504X, 011014.1-011014.7Article

Designing Low Pressure Turbines for Optimized Airfoil LiftGIER, Jochen; FRANKE, Matthias; HÜBNER, Norbert et al.Journal of turbomachinery. 2010, Vol 132, Num 3, issn 0889-504X, 031008.1-031008.12Article

Establishing a Methodology for Resolving Convective Heat Transfer From Complex GeometriesOSTANEK, Jason K; PRAUSA, J; VAN SUETENDAEL, A et al.Journal of turbomachinery. 2010, Vol 132, Num 3, issn 0889-504X, 031014.1-031014.10Article

Blade Tip Clearance Flow and Compressor Nonsynchronous Vibrations : The Jet Core Feedback Theory as the Coupling MechanismTHOMASSIN, Jean; HUU DUC VO; MUREITHI, Njuki W et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011013.1-011013.9Article

Film-Cooling Effectiveness on a Rotating Blade PlatformSURYANARAYANAN, A; MHETRAS, S. P; SCHOBEIRI, M. T et al.Journal of turbomachinery. 2009, Vol 131, Num 1, issn 0889-504X, 011014.1-011014.12Article

Mass/Heat Transfer in Rotating, Smooth, High-Aspect Ratio (4:1) Coolant Channels With Curved WallsSETHURAMAN, Eashwar; ACHARYA, Sumanta; NIKITOPOULOS, Dimitris E et al.Journal of turbomachinery. 2009, Vol 131, Num 2, issn 0889-504X, 021002.1-021002.9Article

Film-Cooling Flowfields With Trenched Holes on an EndwallSUNDARAM, N; THOLE, K. A.Journal of turbomachinery. 2009, Vol 131, Num 4, issn 0889-504X, 041007.1-041007.10Article

Simplified Approach to Predicting Rough Surface TransitionBOYLE, R. J; STRIPF, M.Journal of turbomachinery. 2009, Vol 131, Num 4, issn 0889-504X, 041020.1-041020.11Article

Boundary Layer Transition on the High Lift T106A Low-Pressure Turbine Blade With an Oscillating Downstream Pressure FieldOPOKA, Maciej M; THOMAS, Richard L; HODSON, Howard P et al.Journal of turbomachinery. 2008, Vol 130, Num 2, issn 0889-504X, 021009.1-021009.10Article

Control of Rotor Tip Leakage Through Cooling Injection From the Casing in a High-Work TurbineBEHR, Thomas; KALFAS, Anestis I; ABHARI, Reza S et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031014.1-031014.12Article

Heat Transfer at High Rotation Numbers in a Two-Pass 4:1 Aspect Ratio Rectangular Channel With 45 deg Skewed RibsFUGUO ZHOU; ACHARYA, Sumanta.Journal of turbomachinery. 2008, Vol 130, Num 2, issn 0889-504X, 021019.1-021019.12Article

Numerical Study of Instability Mechanisms Leading to Transition in Separation BubblesMCAULIFFE, Brian R; YARAS, Metin I.Journal of turbomachinery. 2008, Vol 130, Num 2, issn 0889-504X, 021005.1-021005.8Article

The Influence of Sweep on Axial Flow Turbine Aerodynamics in the Endwall RegionPULLAN, Graham; HARVEY, Neil W.Journal of turbomachinery. 2008, Vol 130, Num 4, issn 0889-504X, 041011.1-041011.10Article

The 9th Asian International Conference in Fluid Machinery. AICFM-9KIM, Youn-Jea.Journal of mechanical science and technology. 2008, Vol 22, Num 10, issn 1738-494X, 154 p.Conference Proceedings

Preliminary fan design for a silent aircraftCRICHTON, Daniel; LIPING XU; HALL, Cesare A et al.Journal of turbomachinery. 2007, Vol 129, Num 1, pp 184-191, issn 0889-504X, 8 p.Article

Scaling of guide vane coolant profiles and the reduction of a simulated hot streakJENKINS, Sean C; BOGARD, David G.Journal of turbomachinery. 2007, Vol 129, Num 3, pp 619-627, issn 0889-504X, 9 p.Article

The effect of stagger variability in gas turbine fan assembliesWILSON, Mark J; IMREGUN, Mehmet; SAVMA, Abdulnaser I et al.Journal of turbomachinery. 2007, Vol 129, Num 2, pp 404-411, issn 0889-504X, 8 p.Article

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