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ExCCL Publications

Journal Papers and Conference Proceedings 

Mekki, B., Langer, J., & Lynch, S., “Genetic Algorithm Based Topology Optimization of Heat Exchanger Fins Used in Aerospace Applications.” Proceedings of the 2019 ASME International Mechanical Engineering Congress & Expo, Salt Lake City, UT.

Haydt, S., & Lynch, S., “Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles.” Proceedings of the 2019 ASME IGTI Turbo Expo, Phoenix, AZ.

Zuccarello, J., Lange, E., & Lynch, S., “Effect of Longitudinal Vortices on Turbulent Junction Flow Heat Transfer.” Proceedings of the 2019 AIAA Propulsion and Energy Conference, Indianapolis, IN.

Haydt, S., & Lynch, S., “Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles.” J. Turbomach., 141(4), 2019.

Elahi, S., Lange, E., & Lynch, S., “Experimental Measurements of Turbulent Junction Flow Using High Speed Stereo PIV and IR Thermography.” International Journal of Heat and Mass Transfer, Vol. 142, 2019.

Bichnevicius, M., Saltzman, D., & Lynch, S., “Comparison of Additively Manufactured Louvered Plate-Fin Heat Exchangers.” Journal of Thermal Science and Engineering Applications, 12(1), 2019.

Haydt, S., & Lynch, S., “Flowfield of a Shaped Film Cooling Hole Over a Range of Compound Angles.” Proceedings of the 2018 ASME IGTI Turbo Expo, Lillestrom, Norway.

Haydt, S., & Lynch, S., “Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles.” Proceedings of the 2018 ASME IGTI Turbo Expo, Lillestrom, Norway.

Lynch, S., “Large Eddy Simulations of Low Pressure Turbine Endwall Flow and Heat Transfer.” Proceedings of the 2018 ASME International Mechanical Engineering Congress & Expo, Pittsburgh, PA.

Bichnevicius, M., Saltzman, D., & Lynch, S., “Comparison of Louvered Plate-Fin heat Exchangers Made via Additive Manufacturing.” Proceedings of the 2018 ASME International Mechanical Engineering Congress & Expo, Pittsburgh, PA.

Saltzman, D., Bichnevicius, M., Lynch, S., Simpson, T. W., Reutzel, E., Dickman, C., & Martukanitz, R., “Experimental Comparison of a Traditionally Built Versus Additively Manufactured Aircraft Heat Exchanger.” Applied Thermal Engineering, Vol. 138, pp. 254-263, 2018.

Muirhead, K., & Lynch, S., “A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes.” Journal of Propulsion and Power, 35(1), 2018.

Elahi, S. S., Moul, Z. K., Lange, E. A., and Lynch, S. P., “Unsteady Heat Flux Measurements of Junction Flow With Reynolds Number and Freestream Turbulence Effects,” Proceedings of the 2018 AIAA SciTech Conference, Kissimmee, FL.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes with Constant Expansion Angles,” J. Turbomach. , 140(5), p. 051002, 2018.

Lange, E. A., Elahi, S. S., and Lynch, S. P., “Time-resolved PIV Measurements of the Effect of Freestream Turbulence on Horseshoe Vortex Dynamics,” Proceedings of the 2018 AIAA SciTech Conference, Kissimmee, FL.

Saltzman, D., Bichnevicius, M., Lynch, S. P., Simpson, T. W., Reutzel, E. W., Dickman, C., and Martukanitz, R., “Experimental Comparison of a Traditionally Built versus Additively Manufactured Aircraft Heat Exchanger,” Proceedings of the 2017 AIAA SciTech Conference, Grapevine TX.

Muirhead, K. and Lynch, S. P., “A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes,” Proceedings of the 2017 AIAA SciTech Conference, GrapeVine, TX.

Leonetti, M., Lynch, S. P., O’Connor, J., and Bradshaw S., “Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield,” Journal of Propulsion and Power , vol. 33, no. 3, pp. 750-763, 2017.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness,” J. Turbomach. , 139(9), p. 091012, 2017.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes with Constant Expansion Angles,” Conference Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, Charlotte, S. C., GT2017-63692.

Elahi, S. S., Lange, E. A., and Lynch S. P., “Experimental Measurements of Turbulent Junction Flow Using High Speed Stereo PIV and IR Thermography,” Proceedings of the 2017 AIAA Aviation Conference, Denver, CO.

Lynch, S. P., “Three-Dimensional Boundary Layer in a Turbine Blade Passage,” Journal of Propulsion and Power, vol. 33, No. 4, pp. 954-963, 2017.

Siroka, S., Shallcross, M., Lynch, S. P., 2016, “Unsteady Heat Transfer Around Low Aspect Ratio Cylinders in an Array,” ASME paper IMECE2016-66783, Conference proceedings of the 2016 ASME International Mechanical Engineering Congress and Expo, Phoenix, Arizona, USA.

Lynch, S. P., 2016, “Measurements and Predictions of the Three-Dimensional Boundary Layer in a Turbine Blade Passage,” AIAA paper 2016-1891, Conference Proceedings of the 2016 AIAA SciTech Conference, San Diego, CA, USA.

Anderson, C. D., Lynch, S. P., “Time-resolved stereo PIV measurements of the horseshow vortex system at multiple locations in a low-aspect pin-fin array,” Experiments in Fluids, vol. 57, pp. 1-18, 2016.

Lange, E., Lynch, S. P., Lewis, S., “Computational and Experimental Studies of Midpassage Gap Leakage and Misalignment for a Non-Axisymmetric Contoured Turbine Blade Endwall,” ASME paper GT2016-56128, Conference Proceedings of the 2016 ASME IGTI Turbo Expo, Seoul, South Korea.

Haydt, S., Lynch, S. P., Lewis, S., “The Effect of Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness,” ASME paper GT2016-56135, Conference Proceedings of the 2016 ASME IGTI Turbo Expo, Seoul, South Korea.

Anderson, C., Lynch, S., 2015, “Time Resolved Stereo-PIV Measurements of the Horseshoe Vortex System in a Low Aspect Ratio Pin-Fin Array,” AIAA paper 2015-3373, Conference Proceedings of the 2015 AIAA Propulsion and Energy Conference, Orlando, FL USA.

Lynch, S. P., Thole, K.A., 2015, “Heat Transfer and Film Cooling on a Contoured Blade Endwall with Platform Gap Leakage,” ASME paper GT2015-43301, Conference Proceedings of the 2015 ASME IGTI Turbo Expo, Montreal, Canada.

Lynch, S. P., Thole, K.A., 2015, “Comparison of the Three-Dimensional Boundary Layer on Flat versus Contoured Turbine Endwalls,” ASME paper GT2015-43298, Conference Proceedings of the 2015 ASME IGTI Turbo Expo, Montreal, Canada.

Milanovic, I., Whiton, J., Florea, R., Lynch, S., Tillman, G., Stucky, M., 2014, “RANS Simulations for Sensitivity Analysis of Compressor Transition Duct,” AIAA paper 2014-3631, Conference Proceedings of the 2014 AIAA Propulsion and Energy Conference, Cleveland, OH USA.

Lawson, S. A., Lynch, S. P., and Thole, K.A., 2013, “Simulations of Multi-Phase Particle Deposition on a Non-Axisymmetric Contoured Endwall with Film Cooling,” ASME J. of Turbomachinery, Vol. 135, pp. 031032-1-11.

Lynch, S. P., Thole, K.A., Kohli, A., Lehane, C., and Praisner, T., 2013, “Endwall Heat Transfer for a Turbine Blade with an Upstream Cavity and Rim Seal Leakage,” ASME paper GT2013-94942, Conference Proceedings of the 2013 ASME IGTI Turbo Expo, San Antonio, TX USA.

Lynch, S. P., Thole, K.A., Kohli, A., Lehane, C., and Praisner, T., 2013, “Aerodynamic Loss for a Turbine Blade with Endwall Leakage Features and Contouring,” 2013, ASME paper GT2013-94943, Conference Proceedings of the 2013 ASME IGTI Turbo Expo, San Antonio, TX USA.

Lawson, S. A., Lynch, S. P., and Thole, K.A., 2012, “Simulations of Multi-Phase Particle Deposition on a Non-Axisymmetric Contoured Endwall with Film Cooling,” ASME paper GT2012-68174, Conference Proceedings of the 2012 ASME IGTI Turbo Expo, Copenhagen, Denmark.

 

Lynch, S. P., Thole, K. A., Kohli, A., and Lehane, C., “Computational Predictions of Heat Transfer and Film-Cooling for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” J Turbomach, vol. 133, pp. 041003, 2011.

Lynch, S. P., Sundaram, N., Thole, K. A., Kohli, A., and Lehane, C., “Heat Transfer for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” J Turbomach, vol. 133, 011019, 2011.

Lynch, S. P. and Thole, K. A., 2011, “The Effect of the Combustor-Turbine Slot and Mid-Passage Gap on Vane Endwall Heat Transfer,” ASME J. of Turbomachinery, Vol. 133, pp. 041002-1-9.

Lynch, S. P., Thole, K. A., Kohli, A., and Lehane, C., 2010, “Computational Predictions of Heat Transfer and Film Cooling for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” ASME paper GT2010-22984, Conference Proceedings of the 2010 ASME IGTI Turbo Expo, Glasgow, Scotland.

Lynch, S. P., Narayan, S., Thole, K. A., Kohli, A., and Lehane, C., 2009, “Heat Transfer for a Turbine Blade with Non-Axisymmetric Endwall Contouring,” ASME paper GT2009-60185, Conference Proceedings of the 2009 ASME IGTI Turbo Expo, Orlando, Florida, USA.

Lynch, S. P. and Thole, K. A., 2009, “The Effect of the Combustor-Turbine Slot and Mid-Passage Gap on Vane Endwall Heat Transfer,” ASME paper IMECE2009-12847, Conference Proceedings of the 2009 ASME International Mechanical Engineering Congress and Expo, Orlando, Florida, USA.

Lynch, S. P. and Thole, K. A., “The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane,” J Turbomach, vol. 130, pp. 041019, 2008.

Lynch, S. P. and Thole, K. A., 2007, “The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane,” ASME paper GT2007-27867, Conference Proceedings of the 2007 ASME IGTI Turbo Expo, Montreal, Canada.

Haydt, S., & Lynch, S., “Flowfield of a Shaped Film Cooling Hole Over a Range of Compound Angles.” Proceedings of the 2018 ASME IGTI Turbo Expo, Lillestrom, Norway.

Haydt, S., & Lynch, S., “Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles.” Proceedings of the 2018 ASME IGTI Turbo Expo, Lillestrom, Norway.

Lynch, S., “Large Eddy Simulations of Low Pressure Turbine Endwall Flow and Heat Transfer.” Proceedings of the 2018 ASME International Mechanical Engineering Congress & Expo, Pittsburgh, PA.

Bichnevicius, M., Saltzman, D., & Lynch, S., “Comparison of Louvered Plate-Fin heat Exchangers Made via Additive Manufacturing.” Proceedings of the 2018 ASME International Mechanical Engineering Congress & Expo, Pittsburgh, PA.

Saltzman, D., Bichnevicius, M., Lynch, S., Simpson, T. W., Reutzel, E., Dickman, C., & Martukanitz, R., “Experimental Comparison of a Traditionally Built Versus Additively Manufactured Aircraft Heat Exchanger.” Applied Thermal Engineering, Vol. 138, pp. 254-263, 2018.

Muirhead, K., & Lynch, S., “A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes.” Journal of Propulsion and Power, 35(1), 2018.

Elahi, S. S., Moul, Z. K., Lange, E. A., and Lynch, S. P., “Unsteady Heat Flux Measurements of Junction Flow With Reynolds Number and Freestream Turbulence Effects,” Proceedings of the 2018 AIAA SciTech Conference, Kissimmee, FL.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes with Constant Expansion Angles,” J. Turbomach. , 140(5), p. 051002, 2018.

Lange, E. A., Elahi, S. S., and Lynch, S. P., “Time-resolved PIV Measurements of the Effect of Freestream Turbulence on Horseshoe Vortex Dynamics,” Proceedings of the 2018 AIAA SciTech Conference, Kissimmee, FL.

Saltzman, D., Bichnevicius, M., Lynch, S. P., Simpson, T. W., Reutzel, E. W., Dickman, C., and Martukanitz, R., “Experimental Comparison of a Traditionally Built versus Additively Manufactured Aircraft Heat Exchanger,” Proceedings of the 2017 AIAA SciTech Conference, Grapevine, TX.

Muirhead, K. and Lynch, S. P., “A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes,” Proceedings of the 2017 AIAA SciTech Conference, Grapevine, TX.

Leonetti, M., Lynch, S. P., O’Connor, J., and Bradshaw S., “Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield,” Journal of Propulsion and Power , vol. 33, no. 3, pp. 750-763, 2017.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of a Meter-Diffuser Offset on Shaped Film Cooling Hole Adiabatic Effectiveness,” J. Turbomach. , 139(9), p. 091012, 2017.

Haydt, S., Lynch, S. P., and Lewis S., “The Effect of Area Ratio Change Via Increased Hole Length for Shaped Film Cooling Holes with Constant Expansion Angles,” Conference Proceedings of the ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, Charlotte, S. C., GT2017-63692.

Elahi, S. S., Lange, E. A., and Lynch S. P., “Experimental Measurements of Turbulent Junction Flow Using High Speed Stereo PIV and IR Thermography,” Proceedings of the 2017 AIAA Aviation Conference, Denver, CO.

Lynch, S. P., “Three-Dimensional Boundary Layer in a Turbine Blade Passage,” Journal of Propulsion and Power, vol. 33, No. 4, pp. 954-963, 2017.