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=DNS Channel Flow= ...ofiles of different statistics and Reynolds stress budgets for the channel flow case are available in <code>.h5</code> format which can be accessed using [

=DNS Channel Flow <math>Re_\tau</math>=180= ...l canonical flow. The simulation was undertaken using the open source PyFR flow solver on Nvidia V100 GPUs on the [https://www.hpc.cineca.it/hardware/marco

=DNS Channel Flow= ...d to study turbulence in wall bounded turbulence. DNS of turbulent channel flow were undertaken at <math>Re_\tau=180</math>.

=DNS Channel Flow= ...le in the [http://kbwiki-data.s3-eu-west-2.amazonaws.com/index.html?prefix=DNS-1/2/Channel_180/snapshots/ database]. The snapshots are acquired at every 5

=DNS Channel Flow= ...an overview of the numerical method/setup used for the computation of the DNS or

=DNS Channel Flow= ...le in the [http://kbwiki-data.s3-eu-west-2.amazonaws.com/index.html?prefix=DNS-1/2/Channel_180/statistics/ database]. The database consists of the budgets

=Flow in a 3D diffuser= ...ber of 10000 is considered based on the duct height and bulk velocity. The flow is considered to be incompressible.

==February 2024: Update to AC 1-05 Ahmed body flow== AC 1-05 [[AC_1-05|Ahmed body flow]] has been updated with new LES results added.

...des details of the solution accuracy obtained by tackling the rounded step DNS with MIGALE. It is commonly accepted that DNS requirements are achieved when <math>{\Delta}/{\eta_{K}}\leq 5</math>.

...tails of the solution accuracy obtained by tackling the wing-body junction DNS with MIGALE. ...nes have been extracted within the highly resolved region of the turbulent flow, see [[DNS_1-6_Quantification_of_Resolution_#figure7|Fig. 7]].

=Flow in a 3D diffuser= ...present grid is at DNS level. In particular, it is commonly accepted that DNS is achieved when <math>{\Delta/\eta_K \leq 5}</math>, as shown in [[lib:DNS

= Cylinder-wall junction flow = == Underlying Flow Regime 3-35 ==

=DNS Channel Flow= ...(first solution point) to <math>\Delta y^+=4.6</math> at the centre of the channel. The near-wall Kolmogorov length scale, <math>\eta=\left(\bar{\rho}\nu^3/\e

= 2D flow over backward facing step  = Underlying Flow Regime 3-15 <font size="-2" color="#888888">               © copy

= 2D flow over backward facing step  = Underlying Flow Regime 3-15 <font size="-2" color="#888888">               © copy

=Flow in a 3D diffuser= ...flow from the compressor to adapt for the combustor section. The following DNS data has been obtained using the in-house Finite Element Method (FEM) code

Underlying Flow Regime 3-30 ...ng, B.: Experimental and theoretical investigation of backward-facing step flow, J. Fluid Mech. vol. 127, pp. 473-496

=Cylinder-wall junction flow= == Underlying Flow Regime 3-35 ==

=Flow in a 3D diffuser= ===Underlying Flow Regime 4-16===