Direct numerical simulation of complete transition to turbulence via oblique breakdown at Mach 3

By Christian S. J. Mayer, Dominic von Terzi, Hermann F. Fasel. Journal of Fluid Mechanics, 2011

132 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/cf66dbf2cbee9d5606d9803e9fcda038cd7e0745

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. Sanjiva K. Lele
2. Kenneth J. Franko
3. Christoph Hader
4. Hermann F. Fasel
5. Christophe Bogey
6. Christophe Bailly
7. Sergio Pirozzoli
8. Tim Colonius

In Computational Mechanics

1. Christoph Hader
2. Sanjiva K. Lele
3. Kenneth J. Franko
4. Hermann F. Fasel
5. Tim Colonius
6. Christophe Bailly
7. Christophe Bogey
8. Sergio Pirozzoli

Citations in the corpus

• Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown (2019, methodology): “…wall units obtained for the fundamental breakdown DNS are comparable to the wall units used to resolve a turbulent boundary layer for a flat plate at Mach 3 (Mayer et al. 2011), suggesting that the grid resolution was adequate to capture the main effects of the laminar–turbulent transition process.”
• Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers (2013, methodology): “Mayer et al. (2011) computed in detail the transition of a Mach 3.0 boundary layer due to oblique breakdown.”