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Lynch, Stephen
Background in convective heat transfer and aerodynamics, specifically for gas turbine engines and power generation. Spent 2 years at United Technologies Research Center (Senior Research Engineer, Aerodynamics) leading industrial research projects on gas turbine efficiency improvements before coming to Penn State.

 

Publications
 
Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring  Journal of Turbomachinery 133 (4), 041003, 2011
Heat transfer for a turbine blade with nonaxisymmetric endwall contouring  Journal of Turbomachinery 133 (1), 011019, 2011
Simulations of Multiphase Particle Deposition on a Nonaxisymmetric Contoured Endwall With Film-Cooling  Journal of Turbomachinery 135 (3), 031032, 2013
The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane  Journal of Turbomachinery 130 (4), 041019, 2008
The effect of the combustor-turbine slot and midpassage gap on vane endwall heat transfer  Journal of Turbomachinery 133 (4), 041002, 2011
 
Resources
 
Skills
 
Combustion
Heat Transfer
Power Systems
Propulsion and Power Generation
Thermal Science and Materials
Institute
 
Institute for Natural Gas Research