New Experimental Data of STBLI at DNS/LES Accessible Reynolds Numbers
By Patrick Bookey, Christopher Wyckham, Alexander J Smits, M. Pino Martín. 2005
150 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/3f1ace81eb07f36474bcbfa39c5574d03ad75728
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
- Sergio Pirozzoli
- Matteo Bernardini
- Stefan Hickel
- Vito Pasquariello
- ÍN M.PINOMART
- Nikolaus A. Adams
- M. Pino Martín
- Minwei Wu
In Computational Mechanics
- Sergio Pirozzoli
- Matteo Bernardini
- Nikolaus A. Adams
- M. Pino Martín
- Stefan Hickel
- Sanjiva K. Lele
- Vito Pasquariello
- Minwei Wu
Citations in the corpus
- Turbulence in supersonic boundary layers at moderate Reynolds number (2011, background): “…by mushroomshaped ejections of fluid erupting into the outer, cooler stream, and which bear close similarities with the cloud-like structures visualized with the Rayleigh scattering technique (which effectively educes density variations) by Smith & Smits (1995) and Bookey et al. (2005).”
- Direct numerical simulation of supersonic turbulent boundary layer over a compression ramp (2007, methodology): “The incoming flow conditions are listed in Table 1, including the reference experiment of Bookey et al. [7] for the same flow.”
- Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data (2007, methodology): “They validated the DNS data against the experiments of Bookey et al. (2005) at matching flow conditions, and they illustrated the existence of the superstructures.”
- Unsteady effects of strong shock-wave/boundary-layer interaction at high Reynolds number (2017, methodology): “Priebe, Wu & Martín (2009) studied the case of a Mach 2.9 impinging SWBLI at a Reynolds number of Reδ0 ≈ 38 × 10 3 and deflection angle of 12◦ by means of DNS, matching experimental flow conditions of Bookey et al. (2005).”
- Flow physics and RANS modelling of oblique shock/turbulent boundary layer interaction (2013, background): “…of high-quality experiments have recently been carried out to investigate OSTBLI by groups at Princeton University (Bookey, Wyckham & Smits 2005a; Bookey et al. 2005b), the Delft University of Technology (TUD) (Humble, Scarano & van Oudheusden 2007; Humble et al. 2009a,b), the University of…”