Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation

By Sergio Pirozzoli, Matteo Bernardini, Francesco Grasso. Journal of Fluid Mechanics, 2010

163 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/3b5210ad5d9e5b33e22db4236b7c12c62042aff5

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. Sergio Pirozzoli
2. Matteo Bernardini
3. E. Touber
4. Neil D. Sandham

In Computational Mechanics

1. Sergio Pirozzoli
2. Matteo Bernardini
3. Sanjiva K. Lele
4. Chi-Wang Shu
5. Francesco Grasso
6. Yiqing Shen
7. Nikolaus A. Adams
8. Johan Larsson

Citations in the corpus

• Numerical Methods for High-Speed Flows (2011, methodology): “…of shock sensors in practical computations can be appreciated from inspection of Figure 4, where we report results of application of some of the indicators previously mentioned to the instantaneous flow field obtained from DNS of transonic shock/boundary layer interaction (Pirozzoli et al., 2010).”