History effects and near equilibrium in adverse-pressure-gradient turbulent boundary layers

By A. Bobke, Ricardo Vinuesa, Ramis Örlü, Philipp Schlatter. Journal of Fluid Mechanics, 2017

212 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/88ac0fa5cc4c20deb612d0fb8ed99d8bbc3d52bd

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. Philipp Schlatter
2. Ricardo Vinuesa
3. Dan S. Henningson
4. Luca Brandt
5. Tamer A. Zaki

In Computational Mechanics

1. Ricardo Vinuesa
2. Philipp Schlatter
3. Dan S. Henningson
4. A. Hanifi
5. M. Atzori
6. P. Negi
7. Steven L. Brunton
8. Ramis Örlü

In Mechanical Engineering

1. Ricardo Vinuesa
2. Dan S. Henningson
3. Philipp Schlatter
4. A. Hanifi
5. M. Atzori
6. P. Negi
7. Ramis Örlü
8. Luca Brandt

Citations in the corpus

• Turbulent boundary layers around wing sections up to Rec=1,000,000 (2018, methodology): “These so-called near-equilibrium conditions (Dixit and Ramesh, 2009; Bobke et al., 2017) are obtained when the freestream velocity is described in terms of the streamwise coordinate by a power law, given certain restrictions in the exponent (Townsend, 1956). The work by Townsend (1956) was complemen”