A detailed analysis of film-cooling physics: Part I -- Streamwise injection with cylindrical holes

By D. K. Walters, J. Leylek. 2000

264 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/55e732dcb3f0f09f76653ef39799a64cae4b9f8b

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. Ki-Don Lee
2. Kwang‐Yong Kim

In Computational Mechanics

1. Kwang‐Yong Kim
2. Ki-Don Lee
3. Dong-Yoon Shin

Citations in the corpus

• Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: Part I effectiveness (2003, background): “Induction lift is generated when the two counter-rotating vortices are in close proximity of each other, and these vortices are known to have a detrimental effect on film cooling performance [23].”
• Optimization of a Cylindrical Film Cooling Hole using Surrogate Modeling (2009, background): “Walters and Leylek [ 2 ] performed numerical and experimental investigations of flow field with cylindrical holes by analyzing vortical motions.”