• 263 Citations
  • 8 h-Index
20072019
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Research Output 2007 2019

  • 263 Citations
  • 8 h-Index
  • 25 Conference contribution
  • 15 Article
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Article
2019

Cooling effectiveness for a shaped film cooling hole at a range of compound angles

Haydt, S. & Lynch, S. P., Apr 1 2019, In : Journal of Turbomachinery. 141, 4, 041005.

Research output: Contribution to journalArticle

Cooling
Blow molding
Coolants
Computational fluid dynamics
Heat transfer coefficients

Effect of Reynolds number on turbulent junction flow fluid dynamics and heat transfer

Elahi, S. S., Lange, E. A. & Lynch, S. P., Oct 1 2019, In : International Journal of Heat and Mass Transfer. 142, 118328.

Research output: Contribution to journalArticle

fluid dynamics
Fluid dynamics
Reynolds number
heat transfer
Heat transfer
2018
3 Citations (Scopus)

Design and evaluation of an additively manufactured aircraft heat exchanger

Saltzman, D., Bichnevicius, M., Lynch, S. P., Simpson, T. W., Reutzel, E. W., Dickman, C. & Martukanitz, R., Jun 25 2018, In : Applied Thermal Engineering. 138, p. 254-263 10 p.

Research output: Contribution to journalArticle

3D printers
Heat exchangers
Aircraft
Geometry
Heat transfer
2 Citations (Scopus)

The effect of area ratio change via increased hole length for shaped film cooling holes with constant expansion angles

Haydt, S., Lynch, S. P. & Lewis, S., May 1 2018, In : Journal of Turbomachinery. 140, 5, 051002.

Research output: Contribution to journalArticle

Blow molding
Cooling
Coolants
Momentum
Velocity measurement
2017
3 Citations (Scopus)

Combustor dilution hole placement and its effect on the turbine inlet flowfield

Leonetti, M., Lynch, S. P., O'Connor, J. A. & Bradshaw, S., Jan 1 2017, In : Journal of Propulsion and Power. 33, 3, p. 750-763 14 p.

Research output: Contribution to journalArticle

turbines
combustion chambers
Combustors
turbine
Dilution
6 Citations (Scopus)

Heat Transfer and film cooling on a contoured blade endwall with platform gap leakage

Lynch, S. P. & Thole, K. A., May 1 2017, In : Journal of Turbomachinery. 139, 5, 051002.

Research output: Contribution to journalArticle

Turbomachine blades
Heat transfer
Cooling
Seals
Turbines
4 Citations (Scopus)

The effect of a meter-diffuser offset on shaped film cooling hole adiabatic effectiveness

Haydt, S., Lynch, S. P. & Lewis, S., Sep 1 2017, In : Journal of Turbomachinery. 139, 9, 091012.

Research output: Contribution to journalArticle

Cooling
Blow molding
Coolants
Electric discharge machining
Gas turbines
1 Citation (Scopus)

Three-dimensional boundary layer in a turbine blade passage

Lynch, S. P., Jan 1 2017, In : Journal of Propulsion and Power. 33, 4, p. 954-963 10 p.

Research output: Contribution to journalArticle

three dimensional boundary layer
turbine blades
turbine
Turbomachine blades
Boundary layers
2016
12 Citations (Scopus)
Boundary layers
Turbines
Vortex flow
Heat transfer
Friction
8 Citations (Scopus)

Time-resolved stereo PIV measurements of the horseshoe vortex system at multiple locations in a low-aspect-ratio pin–fin array

Anderson, C. D. & Lynch, S. P., Jan 1 2016, In : Experiments in Fluids. 57, 1, p. 1-18 18 p., 5.

Research output: Contribution to journalArticle

horseshoe vortices
low aspect ratio
particle image velocimetry
Aspect ratio
Vortex flow
2013
11 Citations (Scopus)

Simulations of multiphase particle deposition on a nonaxisymmetric contoured endwall with film-cooling

Lawson, S. A., Lynch, S. P. & Thole, K. A., Mar 25 2013, In : Journal of Turbomachinery. 135, 3, 031032.

Research output: Contribution to journalArticle

Cooling
Secondary flow
Aerodynamics
Turbines
Turbine components
2011
39 Citations (Scopus)

Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring

Lynch, S. P., Thole, K. A., Kohli, A. & Lehane, C., Apr 19 2011, In : Journal of Turbomachinery. 133, 4, 041003.

Research output: Contribution to journalArticle

Turbomachine blades
Turbines
Heat transfer
Cooling
Turbulence models
54 Citations (Scopus)

Heat transfer for a turbine blade with nonaxisymmetric endwall contouring

Lynch, S. P., Sundaram, N., Thole, K. A., Kohli, A. & Lehane, C., Jan 31 2011, In : Journal of Turbomachinery. 133, 1, 011019.

Research output: Contribution to journalArticle

Turbomachine blades
Turbines
Heat transfer
Secondary flow
Geometry
27 Citations (Scopus)
Combustors
Turbines
Heat transfer
Heat transfer coefficients
Cascades (fluid mechanics)
2008
32 Citations (Scopus)
Combustors
Coolants
Heat transfer coefficients
Nozzles
Turbines