• 333 Citations
  • 10 h-Index
20072019

Research output per year

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Research Output

  • 333 Citations
  • 10 h-Index
  • 27 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., Apr 1 2019, In : Journal of Turbomachinery. 141, 4, 041005.

Research output: Contribution to journalArticle

3 Scopus citations

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

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

Research output: Contribution to journalArticle

2018

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

15 Scopus citations

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

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

Research output: Contribution to journalArticle

8 Scopus citations
2017

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

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

Research output: Contribution to journalArticle

4 Scopus citations

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

7 Scopus citations

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

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

Research output: Contribution to journalArticle

5 Scopus citations

Three-dimensional boundary layer in a turbine blade passage

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

Research output: Contribution to journalArticle

3 Scopus citations
2016
13 Scopus citations

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

10 Scopus citations
2013

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

11 Scopus citations
2011

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

46 Scopus citations

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

61 Scopus citations
32 Scopus citations
2008
38 Scopus citations