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Errata to Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages [Journal of Turbomachinery, 134(1), 011012]SALVADORI, Simone; MONTOMOLI, Francesco; MARTELLI, Francesco et al.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, p. 057001.1Article

A Method to Estimate the Performance Map of a Centrifugal Compressor StageCASEY, Michael; ROBINSON, Chris.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021034.1-021034.10Article

A Novel Measuring Technique Utilizing Temperature Sensitive Paint—Measurement Procedure, Validation, Application, and Comparison With Infrared ThermographyLORENZ, M; HORBACH, T; SCHULZ, A et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031003.1-031003.10Article

Analysis of the Unsteady Overtip Casing Heat Transfer in a High Speed TurbineLAVAGNOLI, S; PANIAGUA, G; DE MAESSCHALCK, C et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031027.1-031027.12Article

Boundary Layer Control on a Low Pressure Turbine Blade by Means of Pulsed BlowingMACK, Marion; NIEHUIS, Reinhard; FIALA, Andreas et al.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, 051023.1-051023.8Article

Constrained Adjoint-Based Aerodynamic Shape Optimization of a Single-Stage Transonic CompressorWALTHER, Benjamin; NADARAJAH, Siva.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021017.1-021017.10Article

Detailed Velocity and Turbulence Measurements in an Inclined Large-Scale Film Cooling ArrayEL-GABRY, Lamyaa A; THURMAN, Douglas R; POINSATTE, Philip E et al.Journal of turbomachinery. 2013, Vol 135, Num 6, issn 0889-504X, 061013.1-061013.11Article

Determination of Time Resolved Heat Transfer Coefficient and Adiabatic Effectiveness Waveforms With Unsteady FilmRUTLEDGE, James L; MCCALL, Jonathan F.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021021.1-021021.9Article

Experimental Investigation of a Truncated Pipe Diffuser With a Tandem Deswirler in a Centrifugal Compressor StageKUNTE, Robert; JESCHKE, Peter; SMYTHE, Caitlin et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031019.1-031019.10Article

Experimental Study of Surge Precursors in a High-Speed Multistage CompressorCOURTIADE, Nicolas; OTTAVY, Xavier.Journal of turbomachinery. 2013, Vol 135, Num 6, issn 0889-504X, 061018.1-061018.9Article

Heat Transfer and Pressure Loss in Rectangular One-Side-Ribbed Channels With Different Aspect RatiosKUNSTMANN, Sébastien; VON WOLFERSDORF, Jens; RUEDEL, Uwe et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031004.1-031004.9Article

Improved Trench Film Cooling With Shaped Trench OutletsOGUNTADE, Habeeb Idowu; ANDREWS, Gordon E; BURNS, A. D et al.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021009.1-021009.10Article

Isothermal Boundary Condition at Casing Applied to the Rotor 37 Transonic Axial Flow CompressorBRUNA, Dario; TURNER, Mark G.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 034501.1-034501.4Article

Measurements of Adiabatic Film and Overall Cooling Effectiveness on a Turbine Vane Pressure Side With a TrenchALBERT, Jason E; BOGARD, David G.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, 051007.1-051007.11Article

Numerical Characterization of Pressure Drop Across the Manifold of Turbine Casing Cooling SystemDA SOGHE, Riccardo; ANDREINI, Antonio.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031017.1-031017.9Article

Optimization of a U-Bend for Minimal Pressure Loss in Internal Cooling Channels— Part I: Numerical MethodVERSTRAETE, Tom; COLETTI, Filippo; BULLE, Jérémy et al.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, 051015.1-051015.10Article

Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole PitchDYSON, Thomas E; BOGARD, David G; PIGGUSH, Justin D et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031011.1-031011.8Article

Statistical and Theoretical Models of Ingestion Through Turbine Rim SealsKUNYUAN ZHOU; WOOD, Simon N; OWEN, J. Michael et al.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021014.1-021014.8Article

The Aerothermal Performance of a Cooled Winglet Tip in a High Pressure Turbine CascadeCHAO ZHOU; HODSON, Howard; TIBBOTT, Ian et al.Journal of turbomachinery. 2013, Vol 135, Num 3, issn 0889-504X, 031005.1-031005.10Article

The Effects of Unsteadiness and Compressibility on the Interaction Between Hub Leakage and Mainstream Flows in High-Pressure TurbinesPOPOVIC, Ivan; HODSON, Howard P; JANKE, Erik et al.Journal of turbomachinery. 2013, Vol 135, Num 6, issn 0889-504X, 061015.1-061015.10Article

Time-Dependent Deposition Characteristics of Fine Coal Fly Ash in a Laboratory Gas Turbine EnvironmentLAYCOCK, Robert G; FLETCHER, Thomas H.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021003.1-021003.8Article

Unsteady Interaction Between Annulus and Turbine Rim Seal FlowsCHILLA, Martin; HODSON, Howard; NEWMAN, David et al.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, 051024.1-051024.10Article

A Calculation Tool of a Turbine Cooling Air Schedule for General Gas Turbine Simulation AlgorithmsLALLINI, Valerio; JANIKOVIC, Jan; PILIDIS, Pericles et al.Journal of turbomachinery. 2012, Vol 134, Num 4, issn 0889-504X, 041003.1-041003.8Article

Aeroelasticity at Reversed Flow Conditions — Part II: Application to Compressor SurgeSCHOENENBORN, Harald; BREUER, Thomas.Journal of turbomachinery. 2012, Vol 134, Num 6, issn 0889-504X, 061031.1-061031.8Article

Airfoil Deflection Characteristics During Rub EventsTURNER, Kevin E; DUNN, Michael; PADOVA, Corso et al.Journal of turbomachinery. 2012, Vol 134, Num 1, issn 0889-504X, 011018.1-011018.8Article

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