Tallman, J. A., Haldeman, C. W., Dunn, M. G., Tolpadi, A. K., and Bergholz, R. F., 2009, “Heat Transfer Measurements and Predictions for a Modern, High-Pressure, Transonic Turbine, Including Endwalls,” ASME J. Turbomach., 131 (2), p. 021001.

[CrossRef]Haldeman, C. W., Dunn, M. G., Southworth, S. A., Chen, J. -P., Heitland, G., and Liu, J., 2009, “Time-Accurate Predictions for a Fully Cooled High-Pressure Turbine Stage—Part II: Methodology for Quantifications of Prediction Quality,” ASME J. Turbomach., 131 , p. 031004.

[CrossRef]Haldeman, C. W., Mathison, R. M., Dunn, M. G., Southworth, S., Harral, J. W., and Heitland, G., 2008, “Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine—Part I: Experimental Approach,” ASME J. Turbomach., 130 , p. 021015.

[CrossRef]Haldeman, C. W., Mathison, R. M., Dunn, M. G., Southworth, S., Harral, J. W., and Heitland, G., 2008, “Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine—Part II: Experimental Results and CFD Comparison,” ASME J. Turbomach., 130 , p. 021016.

[CrossRef]Crosh, E., 2008, “Time-Accurate Predictions for the Aerodynamics of a 1 and 1/2 Stage HP Transonic Turbine,” MS thesis, The Ohio State University, Columbus, OH.

Southworth, S. A., Dunn, M. G., Haldeman, C. W., Chen, J. -P., Heitland, G., and Liu, J., 2009, “Time-Accurate Predictions for a Fully Cooled High-Pressure Turbine Stage—Part I: Comparison of Predictions With Data,” ASME J. Turbomach., 131 , p. 031003.

[CrossRef]Rai, M. M., and Dring, R. P., 1990, “Navier–Stokes Analyses of the Redistribution of Inlet Temperature Distortions in a Turbine,” J. Propul. Power, 6 (3), pp. 276–282.

[CrossRef]Rai, M. M., 1987, “Navier–Stokes Simulations of Rotor-Interaction Using Patched and Overlaid Grids,” J. Propul. Power, 3 (5), pp. 387–396.

[CrossRef]Dorney, D. J., Davis, R. L., Edwards, D. D., and Madavan, N. K., 1992, “Unsteady Analysis of Hot Streak Migration in a Turbine Stage,” J. Propul. Power, 8 (2), pp. 520–529.

[CrossRef]Krouthen, B., and Giles, M. B., 1990, “Numerical Investigation of Hot Streaks in Turbines,” J. Propul. Power, 6 (6), pp. 769–776.

[CrossRef]Takahashi, R. K., and Ni, R. H., 1990, “Unsteady Euler Analysis of the Redistribution of an Inlet Temperature Distortion in a Turbine,” The 26th Joint Propulsion Conference , Orlando, FL, Paper No. AIAA 90-2262.

Sharma, O. P., Pickett, G. F., and Ni, R. H., 1990, “Assessment of Unsteady Flows in Turbines,” ASME Paper No. 90-GT-150.

Ni, R. H., and Sharma, O. P., 1990, “Using 3-D Euler Flow Simulations to Assess Effects of Periodic Unsteady Flow Through Turbines,” Paper No. AIAA 90-2357.

Saxer, A. P., and Giles, M. B., 1994, “Predictions of Three-Dimensional Steady and Unsteady Inviscid Transonic Stator/Rotor Interaction With Inlet Radial Temperature Nonuniformity,” ASME J. Turbomach., 116 , pp. 347–357.

[CrossRef]Shang, T., and Epstein, A. H., 1997, “Analysis of Hot Streak Effects on Turbine Rotor Heat Load,” ASME J. Turbomach., 119 , pp. 544–553.

Dorney, D. J., and Schwab, J. R., 1996, “Unsteady Numerical Simulations of Radial Temperature Profile Redistribution in a Single-Stage Turbine,” ASME J. Turbomach., 118 , pp. 783–791.

[CrossRef]Dorney, D. J., and Sondak, D. L., 2000, “Effects of Tip Clearance on Hot Streak Migration in a High-Subsonic Single-Stage Turbine,” ASME J. Turbomach., 122 , pp. 613–620.

[CrossRef]Ong, J., and Miller, R. J., 2008, “Hot Streak and Vane Coolant Migration in a Downstream Rotor,” ASME Paper No. GT2008-50971.

Pau, M., Paniagua, G., Delhaye, D., de la Loma, A., and Ginibre, P., 2008, “Aerothermal Impact of Stator-Rim Purge Flow and Rotor-Platform Film Cooling on a Transonic Turbine Stage,” ASME Paper No. GT2008-51295.

Martelli, F., Adami, P., Salvadori, S., Chana, K. S., and Castillon, L., 2008, “Aero-Thermal Study of the Unsteady Flow Field in a Transonic Gas Turbine With Inlet Temperature Distortions,” ASME Paper No. GT2008-50628.

Dunn, M. G., 2001, “Convective Heat Transfer and Aerodynamics in Axial Flow Turbines,” ASME Paper No. 2001-GT-0506.

Dunn, M. G., Bennett, W., Delaney, R. A., and Rao, K. V., 1990, “Investigation of Unsteady Flow Through a Transonic Turbine Stage: Part II—Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data,” The AIAA/SAE/ASME/ASEE 26TH Joint Propulsion Conference , Orlando, FL, Paper No. AIAA-90-2409.

Erdos, J. I., Alzner, E., and McNally, W., 1977, “Numerical Solution of Periodic Transonic Flow Through a Fan Stage,” AIAA J., 15 (11), pp. 1559–1568.

[CrossRef]Giles, M., and Haimes, R., 1993, “Validation of a Numerical Method for Unsteady Flow Calculations,” ASME J. Turbomach., 115 , pp. 110–117.

[CrossRef]Dawes, W. N., 1992, “The Simulation of Three-Dimensional Viscous Flow in Turbomachinery Geometries Using a Solution-Adaptive Unstructured Mesh Methodology,” ASME J. Turbomach., 114 (3), pp. 528–537.

[CrossRef]Rao, K. V., Delaney, R. A., and Dunn, M. G., 1990, “Investigation of Unsteady Flow Through Transonic Turbine Stage Part I: Analysis,” The AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference , Orlando, FL, Paper No. AIAA-90-2408.

Dunn, M. G., Bennett, W. A., Delaney, R. A., and Rao, K. V., 1992, “Investigation of Unsteady Flow Through a Transonic Turbine Stage: Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data,” ASME J. Turbomach., 114 , pp. 91–99.

[CrossRef]Rao, K. V., Delaney, R. A., and Dunn, M. G., 1994, “Vane-Blade Interaction in a Transonic Turbine, Part I: Aerodynamics,” J. Propul. Power, 10 (3), pp. 305–311.

[CrossRef]Rao, K. V., Delaney, R. A., and Dunn, M. G., 1994, “Vane-Blade Interaction in a Transonic Turbine, Part II: Heat Transfer,” J. Propul. Power, 10 (3), pp. 312–317.

[CrossRef]Abhari, R. S., Guenette, G. R., Epstein, A. H., and Giles, M., 1991, “Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations,” ASME Paper No. 91-GT-190.

Abhari, R. S., 1996, “Impact of Rotor-Stator Interaction on Turbine Blade Film Cooling,” ASME J. Turbomach., 118 , pp. 123–133.

Dunn, M. G., Haldeman, C. W., and Abhari, R. S., 2000, “Influence of Vane/Blade Spacing on the Heat Flux for a Transonic Turbine,” Turbo Expo , Munich, Germany.

Haldeman, C. W., Dunn, M. G., Barter, J. W., Green, B. R., and Bergholz, R. F., 2004, “Aerodynamic and Heat-Flux Measurements With Predictions on a Modern One and 1/2 Stage High Pressure Transonic Turbine,” ASME Paper No. GT2004-53478.

Venable, B. L., Delaney, R. A., Busby, J. A., Davis, R. L., Dorney, D. J., Dunn, M. G., Haldeman, C. W., and Abhari, R. S., 1999, “Influence of Vane-Blade Spacing on Transonic Turbine Stage Aerodynamics: Part I: Time Resolved Data and Analysis,” ASME J. Turbomach., 121 , pp. 663–672.

[CrossRef]Busby, J. A., Davis, R. L., Dorney, D. J., Dunn, M. G., Haldeman, C. W., Abhari, R. S., Venable, B. L., and Delaney, R. A., 1999, “Influence of Vane-Blade Spacing on Transonic Turbine Stage Aerodynamics: Part II: Time Resolved Data and Analysis,” ASME J. Turbomach., 121 , pp. 673–682.

[CrossRef]Barter, J. W., Vitt, P. H., and Chen, J. P., 2000, “Interaction Effects in a Transonic Turbine Stage,” ASME Paper No. 2000-GT-0376.

Adamczyk, J. J., 1985, “Model Equations for Simulating Flows in Multistage Turbomachinery,” NASA Lewis Research Center, Cleveland, OH, Report No. NASA-TM-86869.

Verdon, J. M., and Caspar, J. R., 1982, “Development of a Linear Unsteady Aerodynamic Analysis for Finite-Deflection Subsonic Cascades,” AIAA J., 20 (9), pp. 1259–1267.

[CrossRef]Verdon, J. M., and Caspar, J. R., 1984, “A Linearized Unsteady Aerodynamic Analysis for Transonic Cascades,” J. Fluid Mech., 149 , pp. 403–429.

[CrossRef]Hall, K. C., and Crawley, E. F., 1989, “Calculation of Unsteady Flows in Turbomachinery Using the Linear Euler Equations,” AIAA J., 27 (6), pp. 777–787.

[CrossRef]Hall, K. C., Clark, W. S., and Lorence, C. B., 1994, “A Linearized Euler Analysis of Unsteady Transonic Flows in Turbomachinery,” ASME J. Turbomach., 116 (3), pp. 477–488.

[CrossRef]Ning, W., and He, L., 1998, “Computation of Unsteady Flows Around Oscillating Blades Using Linear and Nonlinear Harmonic Euler Methods,” ASME J. Turbomach., 120 , pp. 508–514.

He, L., and Ning, W., 1998, “Efficient Approach for Analysis of Unsteady Viscous Flows in Turbomachines,” AIAA J., 36 (11), pp. 2005–2012.

[CrossRef]Chen, T., Vasanthakumar, P., and He, L., 2001, “Analysis of Unsteady Blade Row Interaction Using Nonlinear Harmonic Approach,” J. Propul. Power, 17 (3), pp. 651–658.

[CrossRef]Fritsch, G., and Giles, M. B., 1995, “An Asymptotic Analysis of Mixing Loss,” ASME J. Turbomach., 117 , pp. 367–374.

[CrossRef]Aube, M., and Hirsch, C., 2001, “Numerical Investigation of a 1–1/2 Axial Turbine Stage at Quasi-Steady and Fully Unsteady Conditions,” ASME Paper No. 2001-GT-0309.

Vilmin, S., Lorrain, E., Hirsch, C., and Swoboda, M., 2006, “Unsteady Flow Modeling Across the Rotor/Stator Interface Using the Nonlinear Harmonic Method,” ASME Paper No. GT2006-90210.

Gerolymos, G. A., Michon, G. J., and Neubauer, J., 2002, “Analysis and Application of Chorochronic Periodicity in Turbomachinery Rotor/Stator Interaction Computations,” J. Propul. Power, 18 (6), pp. 1139–1152.

[CrossRef]Crosh, E. A., Haldeman, C. W., Dunn, M. G., Holmes, D. G., and Mitchell, B. D., 2009, “Investigation of Turbine Shroud Distortions on the Aerodynamics of a One and One-Half Stage High-Pressure Turbine,” ASME Paper No. GT2009-59562.

Mathison, R. M., Haldeman, C. W., and Dunn, M. G., 2010, “Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine–Part I: Vane Inlet Temperature Profile Generation and Migration,” ASME Paper No. GT2010-22716.

Mathison, R. M., Haldeman, C. W., and Dunn, M. G., 2010, “Aerodynamics and Heat Transfer for a Cooled One and One-Half Stage High-Pressure Turbine—Part II: Influence of Inlet Temperature Profile on Blade Heat Flux,” ASME Paper No. GT2010-22718.

Mathison, R. M., Haldeman, C. W., and Dunn, M. G., 2010, “Heat Transfer for the Blade of a Cooled Stage and One-Half High-Pressure Turbine, Part I: Influence of Vane Cooling and Disk Cavity Purge Flow,” ASME Paper No. GT2010-22713.

Mathison, R. M., Haldeman, C. W., and Dunn, M. G., 2010, “Heat Transfer for the Blade of a Cooled One and One-Half Stage High-Pressure Turbine, Part II: Influence of Purge Cooling Variation,” ASME Paper No. GT2010-22715.