Direct numerical simulation of hypersonic turbulent boundary layers. Part 3. Effect of Mach number

By Lian Duan, I. Beekman, M. Pino Martín. Journal of Fluid Mechanics, 2011

296 citations recorded by the source corpus.

Subfields: Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/2fe0b63a56f0f39fb0524527540deb88a3afcc9e

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. Matteo Bernardini
2. Sergio Pirozzoli
3. You-sheng Zhang
4. Wei-Tao Bi
5. Z. She
6. Fazle Hussain
7. Francesco Grasso
8. Davide Modesti

In Environmental Engineering

1. Matteo Bernardini
2. Sergio Pirozzoli
3. Francesco Grasso

Citations in the corpus

• Turbulence in supersonic boundary layers at moderate Reynolds number (2011, background): “The validity of Morkovin’s density scaling has been addressed in a series of recent studies (Duan et al. 2010, 2011; Lagha et al. 2011), which indicate moderate success in scaling mean and fluctuating velocity distributions across a range of Mach numbers, also in the presence of heated and cooled…”
• A generalized Reynolds analogy for compressible wall-bounded turbulent flows (2013, background): “In the literature, |Ru′T ′ | in quasi-adiabatic flows is found to Generalized Reynolds analogy for compressible wall-bounded turbulent flows 413 be approximately 0.6 ∼ 0.9, significantly deviating from unity (Guarini et al. 2000; Maeder et al. 2001; Pirozzoli et al. 2004; Duan et al. 2011).”