Turbulence in supersonic boundary layers at moderate Reynolds number

By Sergio Pirozzoli, Matteo Bernardini. Journal of Fluid Mechanics, 2011

395 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/e5b932e01e13b71aa8698e31313ed47592d932b9

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

In Computational Mechanics

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

Citations in the corpus

• A generalized Reynolds analogy for compressible wall-bounded turbulent flows (2013, methodology): “For example, the predictions of Ru′T ′ = −1 and Prt = 1 clearly deviate from the observed values of Ru′T ′ =−0.7∼−0.5 and Prt = 0.7∼ 0.9 in quasi-adiabatic CTBLs up to the hypersonic regime (Guarini et al. 2000; Maeder et al. 2001; Pirozzoli et al. 2004; Duan 2011; Pirozzoli & Bernardini 2011).”
• Reynolds and Mach number effects in compressible turbulent channel flow (2016, background): “Hence, it appears that van Driest transformation cannot collapse the entire wall layer, except for the case of an adiabatic wall, since ρ/ρw ≈ 1 in the near-wall region [12].”