Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer

By G. Elsinga, Ronald J. Adrian, B. W. van Oudheusden, Fulvio Scarano. Journal of Fluid Mechanics, 2010

166 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/390e8f46d8e42935487890c4e3fb8e113474ac33

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. Fulvio Scarano
3. Matteo Bernardini
4. T. Nickels
5. G. Elsinga
6. David J. C. Dennis
7. Ivan Marusic
8. B. W. van Oudheusden

In Computational Mechanics

1. Fulvio Scarano
2. Matteo Bernardini
3. T. Nickels
4. Ivan Marusic
5. Sergio Pirozzoli
6. G. Elsinga
7. David J. C. Dennis
8. B. McKeon

In Environmental Engineering

1. T. Nickels
2. David J. C. Dennis
3. B. McKeon
4. Ivan Marusic
5. Sergio Pirozzoli
6. Matteo Bernardini
7. Fulvio Scarano
8. G. Elsinga

Citations in the corpus

• Experimental measurement of large-scale three-dimensional structures in a turbulent boundary layer. Part 2. Long structures (2011, methodology): “This is the same value as used in Elsinga et al. (2007) and is within the range of values used by Elsinga et al. (2010). Figure 7 shows four different iso-surface threshold-level choices.”
• Experimental measurement of large-scale three-dimensional structures in a turbulent boundary layer. Part 1. Vortex packets (2011, background): “…PIV has provided important new information about structures (e.g. Elsinga et al. 2007) – especially at high Reynolds numbers and Mach numbers (Elsinga et al. 2010), the resolution is necessarily limited and the streamwise extent of the interrogation region is also shorter than the full…”
• Tomographic PIV: principles and practice (2012, background): “…first in the low-speed regime (Schröder et al 2008b, Elsinga et al 2007b) and later in high-Reynolds number flows (figure 22, top right) (Reθ = 40 000) and in the supersonic regime (Elsinga et al 2008, 2010a), including the case of shock-wave boundary layer interactions (Humble et al 2009).”
• Turbulence in supersonic boundary layers at moderate Reynolds number (2011, background): “Evidence for clustering of symmetric and asymmetric hairpinlike vortices above low-speed superstructures in supersonic boundary layers was also provided from DNS data at lower Re (Ringuette et al. 2008), and from experiments (Elsinga et al. 2010).”
• Universal aspects of small-scale motions in turbulence (2010, background): “…has subsequently been supported by flow visualizations of 3D velocity data from DNS and experiments (Adrian & Liu 2002; Ringuette, Wu & Martin 2008; Elsinga et al. 2007, 2010) as well as by their signatures observed in planar PIV measurements (Ganapathisubramani, Longmire & Marusic 2003; Tomkins &…”