Publications

Ameri, Ali A., Ajmani, Kumud, "Evaluation of Predicted Heat Transfer on a Transonic Blade Using ν ² – ƒ Models", ASME Paper GT2004-53572, June 2004.

Ameri, A. A., Rigby, D. L., Steinthorsson, E., Gaugler, Raymond, "Computation of Turbulent Heat Transfer on the Walls of a 180 Degree Turn Channel With a Low Reynolds Number Reynolds Stress Model; Final Report", ASME paper 2002-GT-30211, April 2002, also NASA/CR-2002-30211. 

Ameri, Ali A., "Heat Transfer and Flow on the Tip of a Gas Turbine Equipped with a Mean-Camberline Strip", ASME paper 2001-GT-0156, June 2001, NASA/CR—2001-210764.

Ameri, A. A. and Rigby, David L., "A Numerical Analysis of Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models", NASA/CR-1999-209165, July, 1999. Presented at 14th ISABE, Florence, Italy, September 5-10, 1999.

Ameri, A. A. and Bunker, R. S., "Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine, Part 2: Simulation Results", ASME paper 99-GT-283, June, 1999, , also NASA/CR-1999-209151, April, 1999.

Ameri, A. A., Steinthorsson, E. and Rigby, David L., "Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficiency in Axial Turbines", ASME paper 98-GT-369, June, 1998, also NASA/CR-1998-208514, to be published in ASME Journal of Turbomachinery.

Ameri, A. A., Steinthorsson, E. and Rigby, David L., "Effect of Squealer Tip on Rotor Heat Transfer and Efficiency", ASME paper 97-GT-128, June, 1997, & ASME Journal or Turbomachinery, October, 1998, vol. 120, no. 4, pp. 753-759.

Ameri, A. A. and Steinthorsson, E., "Analysis of Gas Turbine Rotor Blade Tip and Shroud Heat Transfer", ASME paper 96-GT-189, June, 1996, also NASA CR 198541, Oct. 1996.

Ameri, A. A. and Steinthorsson, E., "Prediction of Unshrouded Rotor Blade Tip Heat Transfer", ASME paper 95-GT-142, June, 1995, also NASA CR 198542.

Ameri, A. A. and Arnone, A., "Transition Modeling Effects on Turbine Rotor Blade Heat Transfer Predictions", ASME paper 94-GT-22, June, 1994, & ASME Journal of Turbomachinery, April, 1996, vol. 118, no. 2, pp. 307-313.

Ameri, A. A. and Arnone, A., "Prediction of Turbine Blade Passage Heat Transfer Using a Zero and a Two-Equation Turbulence Model", ASME paper 94-GT-122, June, 1994.

Ameri, A. A. and Arnone, A., "Navier-Stokes Turbine Heat Transfer Predictions Using Two-Equation Turbulence Closures", AIAA paper 92-3067, July, 1992, also NASA TM 105817.

Ameri, A. A., Sockol, P. M. and Gorla, R. S. R., "Navier-Stokes Analysis of Turbomachinery Blade external Heat Transfer", Journal of Propulsion and Power Vol. 8. No., March-April 1992.

Ameri, A. A. and Arnone, A., "Three Dimensional Navier-Stokes Analysis of Turbine Passage Heat Transfer", AIAA paper 91-2241, June, 1991.

Azad, Gm S., Han, Je-Chin and Boyle, Robert J., "Heat Transfer and Flow on Squealer Tip of a Gas Turbine Blade", ASME paper 2000-GT-0195, May 2000.

Azad, Gm S., Han, Je-Chin, Teng, Shuye and Boyle, Robert J., "Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip", ASME paper 2000-GT-0194, May 2000.

Boyle, Robert J., "Effects of Thermal Barrier Coatings on Approaches to Turbine Blade Cooling", ASME paper GT2006-91202, May 2006.

Boyle, Robert J., Senyitko, Richard G., "Effects of Surface Roughness on Turbine Vane Heat Transfer", ASME paper GT2005-69133, June 2005. 

Boyle, Robert J., Giel, P. W., and Ames, Forrest E., "Predictions for the Effects of Freestream Turbulence on Turbine Blade Heat Transfer", ASME paper GT2004-54332, NASA/TM-2004-213079, May 2004.

Boyle, Robert J., Senyitko, Richard G., "Measurements and Predictions of Surface Roughness Effects on Turbine Vane Aerodynamics", ASME paper GT-2003-38580.

Boyle, Robert J., Lucci, Barbara L., Senyitko, Richard G., "Aerodynamic Performance and Turbulence Measurements in a Turbine Vane Cascade", ASME paper 2002-GT-30434, May 2002, also NASA/TM-2002-211709, November 2002.

Boyle, Robert J. and Giel, P.W., "Effect of Favorable Pressure Gradients on Turbine Blade Pressure Surface Heat Transfer", NASA/CP-2001-210888, April 2002. 

Boyle, Robert J. and Giel, Paul W., "Prediction of Relaminarization Effects on Turbine Blade Heat Transfer", ASME paper 2001-GT-0162, June 2001.

Boyle , Robert J., Lucci, B.L. and Spuckler, C.M., "Comparison of Predicted and Measured Turbine Vane Rough Surface Heat Transfer", ASME paper 2000-GT-0217, May 2000.

Boyle, Robert J., Lucci, B.L., Spuckler, C.M. and Camperchioli, W.P., "Infrared Low Temperature Turbine Vane Rough Surface Heat Transfer Measurements", ASME paper 2000-GT-0216, May 2000.

Boyle, R. J. and Simon, F. F., "Mach Number Effects on Turbine Blade Transition Length Prediction", ASME paper 98-GT-367, June 1998, also NASA/TM-1998-208404.

Boyle, R. J., Lucci, B. L., Verhoff, V. G., Camperchioli, W. P. and La, H., "Aerodynamics of a Transitioning Stator over a Range of Reynold's Numbers", ASME paper 98-GT-285, June 1998, also NASA/TM-1998-208408.

Boyle, R. J. and Giel, P. W., "Prediction of Nonuniform Inlet Temperature Effects on Vane and Rotor Heat Transfer", ASME paper 97-GT-133, June 1997.

Boyle, R. J. and Lucci, B. L., "Predicted Turbine Heat Transfer for a Range of Test Conditions", ASME paper 96-GT-304, June 1996, also NASA TM 107374, Nov. 1996.

Boyle, R. J. and Jackson, R., "Heat Transfer Predictions for Two Turbine Nozzle Geometries at High Reynolds and Mach Number", ASME Paper 95-GT-104, June, 1995, & ASME Journal of Turbomachinery, vol. 119, no. 2, pp. 270-283, April, 1997.

Boyle, R. J. and Ameri, A. A., "Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance", ASME Paper 94-GT-123, June, 1994.

Boyle, R. J., "Prediction of Incidence and Surface Roughness Effects on Turbine Performance", ASME Paper 93-GT-280, May 1993.

Boyle, R. J. and Giel, P. W., "Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows", AIAA paper 92-3068, July, 1992, also NASA TM-105800,July 1992, & AIAA Journal of Prop. and Power, Vol. 11, No. 6, pp. 1179-1186, 1995.

Boyle, R. J. and Civinskas, K. C., "Two-Dimensional Navier-Stokes Heat Transfer Analysis", NASA-TM-106008.

Boyle, R. J., "Navier-Stokes Analysis of Turbine Blade Heat Transfer", ASME Journal of Turbomachinery, July 1991 Vol. 113 pp. 392-403.

Boyle, R. J. and Russell, L. M., "Experimental Determination of Stator Endwall Heat Transfer", ASME Paper 89-GT-219, and ASME J. of Turbomachinery, July 1990 Vol. 112 pp. 547-558.

Bunker, R. S., Bailey, J. C. and Ameri, A. A., "Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine, Part 1: Experimental Results", ASME paper 99-GT-169, June, 1999, also NASA/CR-1999-209152, April, 1999.

Camci, C., Kim, K., Hippensteele, S. A. and Poinsatte, P. E., "Convection Heat Transfer at the Curved Bottom Surface of a Square to Rectangular Transition Duct Using a New Hue Capturing Based Liquid Crystal Technique", ASME Fundamental Experimental Measurements in Heat Transfer-HTD Vol. 179, pp. 7-22, 1991 and ASME Journal of Heat Transfer (in color), Vol. 115, pp. 311-324.

Camci, C., Kim, K. and Hippensteele, S. A., "A New Hue Capturing Technique for the Quantitative Interpretation of Liquid Crystal Images Used in Convective Heat Transfer Studies", ASME Paper 91-GT-122 and ASME Journal of Turbomachinery, Vol. 114, pp. 765-775, 1992.

Chen, J., Webster, R., Skoch, G. J., Herrick, G. P., Hathaway, M. D., "Technology for Stabalizing the Compression System of a US Army Helicopter Gas Turbine Engine: Validation of Unsteady Simulations", American Helicopter Society, 61st Annual Forum & Technology Display, "New Frontiers in Vertical Flight," Grapevine, TX, June 1-3, 2004.

Chen, S.-C., Veres, J. P., Fitje, J. E., "Turbopump Design and Analysis Approach for Nuclear Thermal Rocket", 2005.

Chima, R. V. and Liou, M.-S., "Comparison of the AUSM+ and H-Cusp Schemes for Turbomachinery Applications", AIAA Paper AIAA-2003-4120, June 2003, also NASA TM-2003-212457.

Chima, R. V., "Calculation of Multistage Turbomachinery Using Steady Characteristic Boundary Conditions", AIAA Paper 98-0968, Jan. 1998, also NASA TM-1998-206613.

Chima, R. V., Giel, P. W. and Boyle, R. J., "An Algebraic Turbulence Model for Three-Dimensional Viscous Flows", NASA TM-105931, presented at the 31st AIAA Aerospace Sciences Meeting, Reno, Nevada, January 11-14, 1993.

Chima, R. V., "Viscous Three-Dimensional Calculations of Transonic Fan Performance", in CFD Techniques for Propulsion Applications, AGARD Conference Proceedings No. CP-510, AGARD, Neuilly-Sur-Seine, France, Feb. 1992, pp 21-1 to 21-19, also NASA TM-103800.

Civinskas, K. C., Boyle, R. J. and McConnaughey, H. V., "Turbine Blading Designed for High Heat Load Space Propulsion Applications", AIAA J. of Propulsion and Power, Sept.-Oct. 1990 Vol. 6 pp. 598-611.

Cully, D., Bright, M. M., Prahst, P. S. and Strazisar, A. J., "Active Flow Separation Control of a Stator Vane Using Surface Injection in a Multistage Compressor Experiment", ASME Paper GT2003-38863, June, 2003, also NASA TM-2003-212356.

Dorney, D. J., Ashpis, David E., Halstead, David E. and Wisler, David C., "Study of Boundary Layer Development in a Two-Stage Low Pressure", AIAA-Journal of Propulsion and Power, vol 16, no 1, pp160-163, February, 2000.

Dorney, Daniel J., Flitan, Horia C., Ashpis, David E. and Solomon, William J., "The Effects of Blade Count on Boundary Layer Development in a Low Pressure Turbine", AIAA-2000-0742, January, 2000, also NASA/TM-2000-209911, Jan. 2000.

Dorney, Daniel J., Lake, James P., King, Paul I. and Ashpis, David E., "Experimental and Numerical Investigation of Losses in Low Pressure Turbine Blade Rows", AIAA-2000-0737, January, 2000, also NASA/TM-2000-209910, Jan. 2000.

Dorney, D. J. and Ashpis, David E., "Study of Low Reynolds Number Effects on the Losses in Low Pressure Turbine Blade rows", International Journal of Turbo and Jet Engines, vol 16, pp91-105, December, 1999.

Dorney, D. J., Ashpis, David E., Halstead, David E. and Wisler, David C., "Study of Boundary Layer Development in a Two-Stage Low Pressure", AIAA-99-0742, January, 1999, also NASA/TM-1999-208913, Feb. 1999.

Dorney, D. J. and Ashpis, David E., "Study of Low Reynolds Number Effects on the Losses in Low Pressure Turbine Blade rows", AIAA-98-3575, July, 1998, also NASA/TM-1998-207919.

Dorney, D. J. and Schwab, J. R., "Unsteady Numerical Simulations of Radial Temperature Profile Redistribution in a Single-Stage Turbine", ASME Paper 95-GT-178, June, 1995.

Dunn, M. G., Kim, J., Civinskas, K. C. and Boyle, R. J., "Time-Averaged Heat Transfer and Pressure Measurements and Comparison with Predictions for a Two-Stage Turbine", ASME Paper 92-GT-194 and ASME J. of Turbomachinery, Jan. 1994 Vol. 116 pp. 14-23.

Garg, Vijay K., "Low-Pressure Turbine Separation Control: Comparison With Experimental Data", NASA/CR-2002-211689.

Garg, Vijay K. and Ameri, Ali A., "Two-Equation Turbulence Models for Prediction of Heat Transfer on a Transonic Turbine Blade", ASME paper 2001-GT-0165, June 2001, NASA/CR-2001-210810.

Garg, V. K., "Heat Transfer in Gas Turbines", NASA CR-2001-210942, March, 2001. Presented at Turbulent Heat Transfer III, Girdwood, Alaska.

Garg, V. K., "Modeling Film-Coolant Flow Characteristics at the Exit of Shower-Head Holes", ASME Paper , NASA/CR-2000-210510, October, 2000.

Garg, V. K., "Heat Transfer on a Film-Cooled Rotating Blade Using Different Turbulence Models", International Journal of Heat and Mass Transfer 42 (1999), pp. 789-802.

Garg, V. K., "Heat Transfer on a Film-Cooled Rotating Blade", ASME Paper 99-GT-044, June, 1999, also NASA/CR-1999-209301, July, 1999.

Garg, V. K. and Rigby, D. L., "Heat transfer on a Film Cooled Blade - Effect of Hole Physics", Int. J. of Heat & Fluid Flow 20 (1999) 10-25.

Garg, V. K., "Heat Transfer on a Film-Cooled Rotating Blade Using a Two-Equation Turbulence Model", International Journal of Rotating Machinery, 1998, Vol. 4, No. 3, pp. 201-216.

Garg, V. K. and Rigby, D. L., "Heat transfer on a Film Cooled Blade - Effect of Hole Physics", ASME Paper 98-GT-404, June, 1998, also NASA/CR-1998-206609. Accepted for publication in Int. J. of Heat & Fluid Flow.

Garg, V. K., "Heat Transfer in Film Cooled Turbine Blades", Proceedings 3rd ISHMT-ASME Heat and Mass Transfer Conference, December, 1997.

Garg, V. K., "Adiabatic Effectiveness and Heat Transfer Coefficient on a Film-Cooled Rotating Blade", In Numerical Heat Transfer, Part A, 32:811-830, 1997.

Garg, V. K. and Abhari, R. S., "Comparison of Predicted and Experimental Nusselt Number for a Film-Cooled Rotating Blade", International Journal of Heat and Fluid Flow, Vol. 18, No. 5, pp. 452-460, 1997.

Garg, V. K. and Ameri, A. A., "Comparison of Two-Equation Turbulence Models for Prediction of Heat Transfer on Film-Cooled Turbine Blades", In Numerical Heat Transfer, Part A, 31:347-371, 1997.

Garg, V. K. and Ameri, A. A., "Comparison of Two-Equation Turbulence Models for Prediction of Heat Transfer on Film-Cooled Turbine Blades", ASME Paper 97-GT-024, June, 1997.

Garg, V. K., "Comparison of Predicted and Experimental Heat Transfer on a Film-Cooled Rotating Blade Using a Two-Equation Turbulence Model", ASME Paper 97-GT-220, June, 1997.

Garg, V. K. and Abhari, R. S., "Comparison of Predicted and Experimental Nusselt Number for a Film-Cooled Rotating Blade", ASME Paper 96-GT-223, June, 1996.

Garg, V. K., "Adiabatic Effectiveness and Heat Transfer Coefficient on a Film-Cooled Rotating Blade", ASME Paper 96-GT-221, June, 1996.

Garg, V. K. and Gaugler, R. E., "Leading Edge Film Cooling Effects on Turbine Blade Heat Transfer", In Numerical Heat Transfer, Part A, 30:165-187, 1996.

Garg, V. K., "Effect of Blade Rotation on Film Cooling of Turbine Blades", Proceedings 2nd ISHMT-ASME Heat and Mass Transfer Conference, pp 595-600, December, 1995.

Garg, V. K. and Gaugler, R. E., "Effect of Coolant Temperature and Mass Flow on Film Cooling of Turbine Blades", ASME Paper 95-WA/HT-1, Nov., 1995; also in International Journal of Heat and Mass Transfer, Vol. 40, No. 2, pp. 435-445, 1997.

Garg, V. K. and Gaugler, R. E., "Leading Edge Film Cooling Effects on Turbine Blade Heat Transfer", ASME Paper 95-GT-275, June, 1995, also NASA TM 106955, June, 1995.

Garg, V. K. and Gaugler, R. E., "Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades", ASME Paper 95-GT-2, June, 1995, & ASME Journal of Turbomachinery, Vol. 119, No. 2, pp. 343-351, April 1997.

Garg, V. K. and Gaugler, R. E., "Prediction of Film Cooling on Gas Turbine Airfoils", ASME Paper 94-GT-16, June, 1994; also NASA TM-10653.

Garg, V. K. and Gaugler, R. E., "Heat Transfer in Film Cooled Turbine Blades", ASME Paper 93-GT-81, May, 1993.

Garg, V. K., "Film Cooled Turbine Vane Heat Transfer", In Proceedings of the IMACS-International Symposium on Scientific Computing and Mathematical Modeling, December, 1992.

Giel, Paul W., Boyle, Robert J., Bunker, Ronald S., "Measurements and Predictions of Heat Transfer on Rotor Blades in a Transonic Turbine Cascade", ASME Paper GT2003-38839, June 2003, ASME J. of Turbomachinery, Vol 126, No. 1, pp.110-121, January 2004

Giel, Paul W., Bunker, Ronald S. , Van Fossen, G. James and Boyle, Robert J., " Heat Transfer Measurements and Predictions on a Power Generation Gas Turbine Blade", ASME paper 2000-GT-0209, May 2000.

Giel P. W., VanFossen, G. J., Boyle, R. J., Thurman, D. R, and Civinskas, K. C., "Blade Heat Transfer Measurements and Predictions in a Transonic Turbine Cascade", ASME 99-GT-125, June, 1999, also NASA/TM-1999-209296.

Giel P. W., Thurman, D. R., Lopez, I., Boyle, R. J. and VanFossen, G. J., Jett, T. A., Camperchioli, W. P. and La, H., "Three-Dimensional Flow Field Measurements in a Transonic Turbine Cascade", ASME 96-GT-113, June, 1996, accepted for publication in the ASME J. of Turbomachinery.

Giel P. W., Thurman, D. R., VanFossen, G. J., Hippensteele, S. A. and Boyle, R. J., "Endwall Heat Transfer Measurements in a Transonic Turbine Cascade", ASME 96-GT-180, June, 1996, recommended for publication in the ASME J. of Turbomachinery.

Giel P. W., Sirbaugh, J. R., Lopez, I. and Van Fossen, G. J., "Three-Dimensional Navier-Stokes Analysis and Redesign of an Imbedded Bellmouth Nozzle in a Turbine Cascade Inlet Section", ASME Paper No. 94-GT-237, June, 1994, & ASME Journal of Turbomachinery, Vol. 118, pp. 529-535, July 1996.

Giel, P. W. and Schmidt, F. W., "A Comparison of Turbulence Modeling Predictions to Experimental Measurements for High Rayleigh Number Natural Convection In Enclosures", Proc. Ninth International Heat Transfer Conference, Jerusalem, Israel, Vol. 2, pp. 175-180, 1990.

Goldman, L. J., "Three-Dimensional Laser Anemometry in Annular Cascades", in Advanced Methods for Cascade Testing, AGARDograph 328, pp. 170-185, August, 1993.

Goldman, L. J., "Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes", NASA TP-3383, July, 1993.

Goldman, L. J. and Seasholtz, R. G., "Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes", NASA TP-3252, July, 1992.

Goldman, L. J., "Three-Component Laser Anemometer Measurement Systems", NASA TP-3080, January, 1991.

Hah, C., Bergner, J. and Schiffer, H.-P., "Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor - Criteria and Mechanisms", ASME Paper GT2006-90045, May, 2006.

Hah, C., Rabe, D. C. and Wadia, A. R., "Role of Tip Leakage Vortices and Paddage Shock in a Swept Transonic Compressor Rotor", ASME Paper GT2004-53867, June, 2004.

Hathaway, M. D., Chen, J. and Webster, R., "Time Accurate Unsteady Simulations of the Stall Inception Process in the Compression System of a U.S. Army Helicopter Gas Turbine Engine", 2004 DOD High Performance Computing Modernization Program User's Group Conference, Bellevue, WA, June 7-10, 2004.

Hathaway, M. D., Chen, J. and Webster, R., "Time Accurate Unsteady Simulations of the Stall Inception Process in the Compression System of a U.S. Army Helicopter Gas Turbine Engine", 2003 DOD High Performance Computing Modernization Program User's Group Conference, Bellevue, WA, June 9-13, 2003.

Hathaway, M. D., "Self Recirculating Casing Treatment Concept for Enhanced Compressor Performance", ASME Paper GT-2002-30368, July, 2002, also NASA TM-2002-211569 or ARL-TR-2748.

Heidmann, James D., Ameri, Ali A., Garg, Vijay K., Rigby, David L., "Improved Modeling Capabilities in GlennHT - The NASA Glenn Research Center General Multi-Block Navier-Stokes Heat Transfer Code", presented at the JANNAF 27th Airbreathing Propulsion Subcommittee Meeting, Colorado Springs, CO, December 2003.

Heidmann, James D., Kasab, Alain J., Divo, Eduardo A., Rodriguez, Franklin, Steinthorsson, Erlendur, "Conjugate Heat Transfer Effects on a Realistic Film-Cooled Turbine Blade", ASME Paper GT2003-38553, June 2003.

Heidmann, James D. and Hunter, Scott D., "Coarse Grid Modeling of Turbine Film Cooling Flows Using Volumetric Source Terms", ASME paper 2001-GT-0138, June 2001.

Heidmann, James D., Rigby, David L. and Ameri, Ali A., "A Three-Dimensional Coupled Internal/External Simulation of a Film-Cooled Turbine Vane", ASME Paper 99-GT-186, June, 1999, also NASA/CR-1999-209078, April, 1999.

Heidmann, James D., Lucci, Barbara L. and Reshotko, Eli, "An Experimental Study of the Effect of Wake Passing on Turbine Blade Film Cooling", ASME Paper 97-GT-255, June, 1997.

Heidmann, James D., "The Effect of Wake Passing on Turbine Blade Film Cooling", NASA TM-107380, Ph.D. Thesis, Case western reserve University, January, 1997.

Heidmann, James D., "A Numerical Study of the Effect of Wake Passing on Turbine Blade Film Cooling", AIAA Paper 95-3044, July 1995.

Heidmann, James D., "Determination of a Transient Heat Transfer Property of Acrylic Using Thermochromic Liquid Crystals", NASA TM-106541, & AIAA Paper 94-0124, January, 1994.

Heidmann, James D., "A Three-Dimensional Navier-Stokes Stage Analysis of the Flow Through a Compact Radial Turbine", NASA TM-104420, & AIAA Paper 91-2564, June, 1991.

Heidmann, James D., "An Analysis of the Viscous Flow Through a Compact Radial Turbine by the Average Passage Approach", NASA TM-102471, & ASME 90-GT-64, June, 1990.

Hippensteele, Steven A., "1996 Coolant Flow Management Workshop", NASA-CP-10195, 1997.

Hippensteele, Steven A., "Film-Cooling Heat-Transfer Measurements Using Liquid Crystals", 1997.

Hippensteele, S. A. and Poinsatte, P. E., "Transient Liquid-Crystal Technique Used to Produce High-Resolution Convective Heat-Transfer-Coefficient Maps", Visualization of Heat Transfer Processes-HTD Vol. xx, pp. x-x; and NASA TM 106083, 1993.

Larosiliere, L. M., Wood, J. R. and Hathaway M. D., "Aerodynamic Design Study of Advanced Multistage Axial Compressor", NASA TP-2002-211568, Dec., 2002, also ARL-TR-2859.

Lau, S. C., Russell, L. M., Thurman, D. R. and Hippensteele, S. A., "Visualization of Local Heat Transfer in Pin Fin Channels with Liquid Crystals", Fifth International Symposium on Transport Phenomena and Dynamics of Rotating Machinery in Maui, Hawaii, May 8-11, 1994; and Journal of Flow Visualization and Image Processing, Vol. 2.

Lau, S. C., Russell, L. M., Thurman, D. R. and Hippensteele, S. A., "Visualization of Local Heat Transfer in a Serpentine Channel with Liquid Crystals", Fifth International Symposium on Transport Phenomena and Dynamics of Rotating Machinery in Maui, Hawaii, May 8-11, 1994.

Lepicovsky, J., Braunscheidel, E. P., Bruckner, R. J., and Tweedt, D. L., "Laser Velocimeter Measurements of Axial Velocity Field in the NASA Supersonic Fan Rotor," ASME Paper 20001-GT-0333, June, 2001.

Lewalle, Jacques, Ashpis, David E. and Sohn, Ki-Hyeon, "Demonstration of Wavelet Techniques in the Spectral Analysis of Bypass Transition Data", NASA TP-3555, December, 1997.

Lewalle, Jacques and Ashpis, David E., "Transport in Bypass Transition: Mapping Active Time Scales using Wavelet Techniques", Tenth Symposium on Turbulent Shear Flows, The Pennsylvania State University, Vol. 2, pp. P2-37 – P2-42, August, 1995.

Lin, Y.-L., Shih, T. I. P., Civinskas, K. C., Rigby, D. L. and Ameri, A. A., "Nonlinear Versus Linear k-w Model for Predicting Flow and Heat transfer in a Smooth U-Duct", AIAA paper AIAA-98-3560, July, 1998.

Merchant, A., Kerrebrock, J. L., Adamczyk. J. J., and Braunscheidel, E., "Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage," ASME Paper GT2004-53679, Sept, 2004. Also NASA TM-2004-213080.

Ng, Daniel and Spuckler, Charles M., "Application of the Self Calibrating Emissivity and/or Transmissivity Independent Multiwavelength Pyrometer to Measure the temperatures of Tungsten and Refractory Material Surfaces", NASA TM 107152, January, 1996.

Ng, Daniel and Spuckler, Charles M., "A Non-Contact Thermal Barrier Coating (TBC) Heat Flux Sensor Using a Self Calibrating Multiwavelength Pyrometer", NASA TM 107150, January, 1996.

Ng, Daniel and Spuckler, Charles M., "Non-Contact Heat Flux Measurement Using a Transparent Sensor", NASA TM 106252, July, 1993.

Rigby, David L. and Bunker, Ronald S., "Heat Transfer in a Complex Trailing Edge Passage for a High Pressure Turbine Blade", NASA/CR-2002-211701, 2002.

Rigby, David L. and Lepicovsky, Jan, "Conjugate Heat Transfer Analysis of Internally Cooled Configurations", ASME paper 2001-GT-0405, June 2001.

Rigby, David L., "Numerical Simulation of Non-Rotating and Rotating Coolant Channel Flow Fields", 2000.

Rigby, David L., "Prediction of Heat and Mass Transfer in a Rotating Ribbed Coolant Passage with a 180 Degree Turn", ASME Paper 98-GT-329, June, 1998, also NASA/TM-1999-208501.

Rigby, David L., Steinthorsson, E. and Ameri, A. A., "Numerical Prediction of Heat Transfer in a Channel with Ribs and Bleed", ASME Paper 97-GT-431, June, 1997.

Rigby, David L., Steinthorsson, E. and Coirier, William J., "Automatic Block Merging Using the Method of Weakest Descent", AIAA Paper 97-0197, January, 1997.

Rigby, David L., Ameri, Ali A. and Steinthorsson, Erlendur, "On the Use of Structured Multi-Block Grids for Internal Coolant Flow Calculations", 1997.

Rigby, David L., "Method of Weakest Descent for Automatic Block Merging", Proceedings of the 15th International Conference of Numerical Methods in Fluid Dynamics, Monterey, CA, June 1996.

Rigby, David L., Ameri, A. A. and Steinthorsson, E., "Internal Passage Heat Transfer Prediction Using Multiblock Grids and a k-w Turbulence Model", ASME Paper 96-GT-188, June, 1996, also NASA CR-198540.

Rigby, David L. and Van Fossen, G. J., "Increased Heat Transfer to Elliptical Leading Edges due to Spanwise Variations in the Freestream Momentum: Numerical and Experimental Results", AIAA Paper 92-3070, July, 1992, also NASA TM-106150.

Rigby, David L. and Van Fossen, G. J., "Increased Heat Transfer to a Cylindrical Leading Edge due to Spanwise Variations in the Freestream Velocity", AIAA Paper 91-1739, June, 1991, also NASA TM-104464.

Russell, L. M., Thurman, D. R., Poinsatte, P. E. and Hippensteele, S. A., "Measurements of Heat Transfer, Flow, and Pressures in a Simulated Turbine Blade Internal Cooling Passage", NASA TP-3646, ARL-TR-923, December, 1997.

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