Flow structure due to dimple depressions on a channel surface

By P. Ligrani, J. L. Harrison, G. I. Mahmmod, M. L. Hill. 2001

266 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/1c0637ad676d9f2abd1d962cea029f3cb9acb575

How researchers see this paper

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

In Computational Mechanics

1. Y. L. He
2. Wen-Quan Tao
3. Phil Ligrani

In Mechanical Engineering

1. Wen-Quan Tao
2. Y. L. He
3. Jianfei Zhang
4. Phil Ligrani

Citations in the corpus

• Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines (2013, background): “The former variations are mostly due to the horseshoe vortices which form at the pin fin/endwall junction [1, 8], whereas the latter are a result of the different vortex structures which are periodically shed from the individual dimples [1, 48, 52].”
• A performance evaluation plot of enhanced heat transfer techniques oriented for energy-saving (2009, background): “Example 4: dimpled surface In the past decade, a new type of enhanced surface, called dimpled surfaces, were extensively studied in the literatures [29–34].”