Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes

By M. Gritsch, W. Colban, Heinz Schaer, K. Döbbeling. 2005

187 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/81aa7408db6a8e1de918c0c10190ab58d07b8539

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Sun-min Kim
2. Robert P. Schroeder
3. Ki-Don Lee
4. Kwang‐Yong Kim
5. K. Thole

In Mechanical Engineering

1. Sun-min Kim
2. Ki-Don Lee
3. Robert P. Schroeder
4. Kwang‐Yong Kim
5. K. Thole
6. M. Moon
7. Dong-Yoon Shin

Citations in the corpus

• Multi-Objective Optimization of a Row of Film Cooling Holes Using an Evolutionary Algorithm and Surrogate Modeling (2013, background): “The low momentum of the coolant coming out from the hole exit resulted in less penetration into the main stream of hot gas, and induced higher film cooling effectiveness [2].”
• ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, methodology): “[3] who tested multiple shaped holes with 7o lateral expansion.”