DNS 1-5 Statistical Data: Difference between revisions

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* turbulent kinetic energy <math>k/u_{ref}^{2}</math>
* turbulent kinetic energy <math>k/u_{ref}^{2}</math>


Profiles at selected streamwise locations are reported in [[Lib:DNS_1-5_statistical#figure10|Fig. 10]].
Profiles at selected streamwise locations are reported in [[Lib:DNS_1-5_statistical#figure11|Fig. 11]].


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<div id="figure10"></div>
<div id="figure11"></div>
{|align="center" border="0" width="600"
{|align="center" border="0" width="600"
|[[Image:DNS1-5 rounded step y u.png|600px]]
|[[Image:DNS1-5 rounded step y u.png|600px]]
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|[[Image:DNS1-5 rounded step y k.png|600px]]
|[[Image:DNS1-5 rounded step y k.png|600px]]
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!align="center"|Figure 10: HiFi-TURB-DLR rounded step, profiles at selected stremwise locations   
!align="center"|Figure 11: HiFi-TURB-DLR rounded step, profiles at selected stremwise locations   
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==Contour data==
==Contour data==
Contour data of averaged velocity components and Reynolds stresses is also provided in [[Lib:DNS_1-5_statistical#figure11|Fig. 11]].
Contour data of averaged velocity components and Reynolds stresses is also provided in [[Lib:DNS_1-5_statistical#figure12|Fig. 12]].
Reynolds stresses show an intensity peak which moves away from the wall as the flow moves above the rounded step.
Reynolds stresses show an intensity peak which moves away from the wall as the flow moves above the rounded step.
Downstream the step, however, such peak gets closer to the wall as the boundary layer is regaining the canonical behaviour for a zero pressure gradient configuration.
Downstream the step, however, such peak gets closer to the wall as the boundary layer is regaining the canonical behaviour for a zero pressure gradient configuration.
Notice that Reynolds stresses <math>R_{zx}</math> and <math>R_{zy}</math> are one order of magnitude smaller than the other Reynolds stresses. This outcome highlights the uncorrelation of streamwise and normalwise velocity fluctuations with respect to spanwise velocity fluctuations.
Notice that Reynolds stresses <math>R_{zx}</math> and <math>R_{zy}</math> are one order of magnitude smaller than the other Reynolds stresses. This outcome highlights the uncorrelation of streamwise and normalwise velocity fluctuations with respect to spanwise velocity fluctuations.


<div id="figure11"></div>
<div id="figure12"></div>
{|align="center" border="0" width="900"
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|[[Image:DNS1-5 rounded step u contour.png|900px]]
|[[Image:DNS1-5 rounded step u contour.png|900px]]
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|[[Image:DNS1-5 rounded step R_zz contour.png|900px]]
|[[Image:DNS1-5 rounded step R_zz contour.png|900px]]
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!align="center"|Figure 11: HiFi-TURB-DLR rounded step, contours of averaged velocity components and Reynolds stresses   
!align="center"|Figure 12: HiFi-TURB-DLR rounded step, contours of averaged velocity components and Reynolds stresses   
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<div id="figure12"></div>
<div id="figure13"></div>
{|align="center" border="0" width="550"
{|align="center" border="0" width="550"
|[[Image:DNS1-5 Rounded step Cp.png|370px]]||[[Image:DNS1-5 Rounded step Cf.png|370px]]
|[[Image:DNS1-5 Rounded step Cp.png|370px]]||[[Image:DNS1-5 Rounded step Cf.png|370px]]
|-
|-
!align="center" colspan="2"|Figure 12: HiFi-TURB-DLR rounded step, pressure and skin friction coefficients on the solid wall   
!align="center" colspan="2"|Figure 13: HiFi-TURB-DLR rounded step, pressure and skin friction coefficients on the solid wall   
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Revision as of 14:54, 13 February 2023


Front Page

Description

Computational Details

Quantification of Resolution

Statistical Data

Instantaneous Data

Storage Format

Statistical data

In this section the relevant statistical data for the flow on the smooth bump computed with MIGALE is given. The reported data is the one mentioned in Table 1 of the list of desirable quantities (PDF).

The data is available as:

  • In .vtk (ASCII) format as statistical data (mid-span plane).
  • In *vtu (ASCII) format for instantaneous data.
  • In CSV (text) format as vertical profiles at various x-positions.

Volume data

Volumetric data on the statistics computed for the whole computational domain are provided here. For more information regarding the stored quantities and the storage format, please refer to the storage format guidelines.

The available files are:

Profile data

Profile data have been extracted at different streamwise locations () and made dimensionless with respect to reference quantities (, , , see UFR 3-36: Table 2). The data stored in each file are:

  • streamwise location
  • vertical location
  • wall distance
  • average pressure
  • average velocity components
  • Reynolds stress components
  • turbulent kinetic energy

Profiles at selected streamwise locations are reported in Fig. 11.

profile_uDNS_-11.00.csv
profile_uDNS_-10.00.csv
profile_uDNS_-09.00.csv
profile_uDNS_-08.00.csv
profile_uDNS_-07.00.csv
profile_uDNS_-06.00.csv
profile_uDNS_-05.00.csv
profile_uDNS_-04.00.csv
profile_uDNS_-03.00.csv
profile_uDNS_-02.00.csv
profile_uDNS_-01.00.csv
profile_uDNS_-00.00.csv
profile_uDNS_+00.50.csv
profile_uDNS_+00.75.csv
profile_uDNS_+01.00.csv
profile_uDNS_+01.25.csv
profile_uDNS_+01.50.csv
profile_uDNS_+01.75.csv
profile_uDNS_+02.00.csv
profile_uDNS_+02.25.csv
profile_uDNS_+02.50.csv
profile_uDNS_+02.75.csv
profile_uDNS_+03.00.csv
profile_uDNS_+03.25.csv
profile_uDNS_+03.50.csv
profile_uDNS_+04.00.csv
profile_uDNS_+04.50.csv
profile_uDNS_+05.00.csv
profile_uDNS_+06.00.csv
profile_uDNS_+07.00.csv
profile_uDNS_+08.00.csv
profile_uDNS_+09.00.csv
profile_uDNS_+10.00.csv
profile_uDNS_+12.00.csv
profile_uDNS_+14.00.csv


DNS1-5 rounded step y u.png
DNS1-5 rounded step y v.png
DNS1-5 rounded step y Rexx.png
DNS1-5 rounded step y Reyx.png
DNS1-5 rounded step y Reyy.png
DNS1-5 rounded step y Rezx.png
DNS1-5 rounded step y Rezy.png
DNS1-5 rounded step y Rezz.png
DNS1-5 rounded step y k.png
Figure 11: HiFi-TURB-DLR rounded step, profiles at selected stremwise locations



Contour data

Contour data of averaged velocity components and Reynolds stresses is also provided in Fig. 12. Reynolds stresses show an intensity peak which moves away from the wall as the flow moves above the rounded step. Downstream the step, however, such peak gets closer to the wall as the boundary layer is regaining the canonical behaviour for a zero pressure gradient configuration. Notice that Reynolds stresses and are one order of magnitude smaller than the other Reynolds stresses. This outcome highlights the uncorrelation of streamwise and normalwise velocity fluctuations with respect to spanwise velocity fluctuations.

DNS1-5 rounded step u contour.png
DNS1-5 rounded step v contour.png
DNS1-5 rounded step R xx contour.png
DNS1-5 rounded step R yx contour.png
DNS1-5 rounded step R yy contour.png
DNS1-5 rounded step R zx contour.png
DNS1-5 rounded step R zy contour.png
DNS1-5 rounded step R zz contour.png
Figure 12: HiFi-TURB-DLR rounded step, contours of averaged velocity components and Reynolds stresses


Additional data

The following averaged quantities are provided along the solid wall:

  • the pressure coefficient
  • the skin friction coefficient

The pressure coefficient is defined as , where is the pressure at wall at the checkpoint , while the skin friction coefficient is defined as . and are the velocity and density at the reference conditions (see UFR 3-36: Table 2), respectively. Both coefficients have been obtained by averaging along the span direction the time averaged solution.

wall_dns.csv
DNS1-5 Rounded step Cp.png DNS1-5 Rounded step Cf.png
Figure 13: HiFi-TURB-DLR rounded step, pressure and skin friction coefficients on the solid wall




Contributed by: Francesco Bassi, Alessandro Colombo, Francesco Carlo Massa — Università degli studi di Bergamo (UniBG)

Front Page

Description

Computational Details

Quantification of Resolution

Statistical Data

Instantaneous Data

Storage Format


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