Index of /turbdata/agard
This data base contains the results of the Working Group 21 of the Fluid
Dynamics Panel of AGARD. It was compiled on October 1997, and it is intended
for the validation of LES computations. As such it contains some data sets,
particularly two-point correlation functions, which are specifically designed
for that purpose. The use of these data is explain in chapter 2 of the
printed report described below.
The companion printed report (AR-345) is available through the standard AGARD (RTO)
channels, and can also be found, in the form of postscript (or PDF) files,
in the directory docs/, from where it can be printed.
This report, and the individual data sheets which it contains, include
much more information on the characteristics of the individual data sets than
is available from the README files in this electronic version. The report
contains, however, no actual data, which can only be found here.
At the time of publication the data base is also available on line at
torroja.dmt.upm.es (Spain) as anonymous ftp
Although both sites are privately maintained, and there is no guarantee
of their permanence, they will probably be updated periodically as new data
become available or bugs are discovered with the present ones.
The data has been examined as thoroughly as possible for errors and
accuracy, but they are otherwise provided "as is". Nevertheless, if you
discover obvious errors, formatting or otherwise, please contact the
member of the working group with whom you feel most comfortable, and we
MAY try to fix it in the on-line sites.
If you REALLY do not know who to contact, send me a mail at:
and I will transfer it to the proper person.
A list of WG members is given at the end of this file.
The data and the printed report are organized into six chapters (3 to 8),
each one dedicated to one class of flows. A summary list of the data chapters
and of the data sets that they contain, is given next.
All the files are ASCII uncoded files, except for a few large ones which
are given in binary, unstructured format, using 32-bits integer or ieeeC
floating point notation (big-endian flavour, as in DEC, IBM, SGI processors).
This data needs to be byte-reversed to be used in Intel chips.
Some utilities are provided for this in the directory progs/, but they may
need adaptation for your particular system. Those data also have to be transferred
with the usual care when going from Unix to Windows systems or vice-versa.
A list of binary files is given below the list of data sets.
Users might particularly want to read chapter 2 of the printed (or *.ps) report
to understand the format and use of these binary files, but each of them
is preceded by an ASCII header that should be read before use.
All binary files are named *.bin.
FILE | FLOW | Experimental (E) or | Authors
| Numerical, DNS (N) |
CHAPTER3: HOMOGENEOUS TURBULENCE
(Isotropic and grid turbulence and their distortions)
chapter3\HOM00 | Decaying grid turbulence | E | Comte-Bellot & Corrsin
chapter3\HOM01 | Decaying grid turbulence | E | Ferchichi & Tavoularis
chapter3\HOM02 | Decaying isotropic turbulence | N | Wray
chapter3\HOM03 | Forced isotropic turbulence | N | Jimenez & Wray
chapter3\HOM04 | Grid turbulence with plane strain | E | Tucker & Reynolds
chapter3\HOM05 | Grid turbulence with transverse strain | E | Leuchter & Benoit
chapter3\HOM06 | Grid turbulence with successive plane strains | E | Gence & Mathieu
chapter3\HOM07 | Return to isotropy of strained grid turbulence | E | Le Penven, Gence & Comte-Bellot
(Rotating turbulence and its distortions)
chapter3\HOM10 | Rotating decaying turbulence | E | Jacquin, Leuchter et al.
chapter3\HOM12 | Rotating turbulence with axisymmetric strain | E | Leuchter & Dupeuple
chapter3\HOM14 | Rotating turbulence with plane strain | E | Leuchter & Benoit
(Sheared turbulence and its distortions)
chapter3\HOM20 | Transversely sheared flow | E | Leuchter et al.
chapter3\HOM21 | Uniformly sheared flow | E | Tavoularis & Corrsin
chapter3\HOM22 | Uniformly sheared flow | E | Tavoularis & Karnik
chapter3\HOM23 | Homogeneous shear flow | N | Rogers & Moin
chapter3\HOM24 | Homogeneous shear flow | N | Sarkar
chapter3\HOM25 | Homogeneous shear flow (high shear) | N | Lee, Kim & Moin
chapter3\HOM26 | Uniformly sheared flow with streamwise
plane strain | E | Sreenivasan
chapter3\HOM27 | Uniformly sheared flow with uniform curvature | E | Holloway & Tavoularis
chapter3\HOM28 | Uniformly sheared flow with S-shaped curvature | E | Chebbi, Holloway & Tavoularis
CHAPTER4: SHOCK-WAVE/ GRID-TURBULENCE INTERACTIONS
chapter4\SHW00 | Stationary shock on grid turbulence | E | Jacquin, Blin & Geffroy
chapter4\SHW01 | Stationary shock on grid turbulence | E | Barre, Alem & Bonnet
CHAPTER5: PIPES AND CHANNELS
chapter5\PCH00 | Pipe | N | Loulou
chapter5\PCH01 | Pipe | E | Durst et al.
chapter5\PCH02 | Pipe | E | Perry et al.
chapter5\PCH03 | Pipe | E | Eggels et al.
chapter5\PCH04 | Super pipe | E | Zagarola
chapter5\PCH05 | Rotating pipe | N | Orlandi & Fatica
chapter5\PCH10 | Channel, Re_tau=400-590 | N | Mansour et al.
chapter5\PCH11 | Channel, Re_tau=921 | E | Niederschulte
chapter5\PCH12 | Channel, Re_tau dependence | E | Wei & Willmarth
chapter5\PCH13 | Channel, High Re | E | Comte-Bellot
chapter5\PCH20 | Rotating channel | E | Johnston et al.
chapter5\PCH21 | Rotating channel | N | Piomelli & Liu
chapter5\PCH22 | Rotating channel | N | Anderson & Kristoffersen
chapter5\PCH23 | Rotating channel | E | Nakabayashi & Kitoh
CHAPTER6: SHEAR LAYERS AND JETS
(Incompressible plane mixing layers)
chapter6\SHL00 | Single stream incomp. M. L. | E | Wygnanski & Fiedler
chapter6\SHL01 | Incompressible M. L., r = 0.6 | E | Bell & Metha
chapter6\SHL02 | Incomp. M. L., 0.5 <= r <= 0.9 | E | Metha
chapter6\SHL03 | Forced incompressible M. L. | E | Oster & Wygnanski
chapter6\SHL04 | Incomp. M. L., r = 0.54 | E | Delville & Bonnet
chapter6\SHL05 | Temporal incomp. M. L. | N | Rogers & Moser
chapter6\SHL06 | Two turb. free streams, r = 0.47 | E | Tavoularis & Corrsin
chapter6\SHL10 | No-shear turbulence mixing | E | Veeravalli & Warhaft
(Compressible Mixing layers)
chapter6\SHL20 | Supersonic M. L., M_c = 0.64; | E | Barre, Menaa, Quine & Dussauge
Re_theta = 1.6x10^4
chapter6\SHL21 | Supersonic M. L., M_c = 0.52; 0.69; 0.87; | E | Elliott & Samimy
Re_theta = 4x10^4
chapter6\SHL22 | Supersonic M. L., M_c = 0.52 -- 1.04; | E | Debisschop, Barre & Bonnet
Re_theta = 8x10^4
chapter6\SHL30 | Round jet | E | Hussein et al.
chapter6\SHL31 | Plane jet | E | Gutmark & Wygnanski
CHAPTER7: BOUNDARY LAYERS
(Zero pressure gradient)
chapter7\TBL00 | Basic flat plate | E | Smith and Smits
chapter7\TBL01 | Pseudo-zero pressure gradient | N | Spalart & Cantwell
(Adverse pressure gradient)
chapter7\TBL10 | APG | E | Marusic & Perry
chapter7\TBL11 | APG | N | Spalart & Watmuff
chapter7\TBL12 | APG | E | Watmuff
chapter7\TBL20 | Closed separation bubble | E | Alving & Fernholz
chapter7\TBL21 | Closed separation bubble | N | Na & Moin.
chapter7\TBL22 | Small heated separation bubble | N | Spalart & Coleman
chapter7\TBL30 | Curved plate | E | Johnson & Johnston
chapter7\TBL31 | Mild bump | E | Webster et al.
CHAPTER8: COMPLEX FLOWS
chapter8\CMP00 | Square duct, UD/nu = 6.5x10^4 | E | Yokosawa et al.
chapter8\CMP01 | Square duct, u_tau D/nu =600 | N | Huser & Biringen
chapter8\CMP10 | Circular cylinder, Re_D=140,000 | E | Cantwell & Coles
chapter8\CMP20 | Square cylinder, Re_D = 22,000 | E | Lyn et al.
chapter8\CMP30 | Backwards facing step, Re_h = 5,100 | N | Le & Moin
chapter8\CMP31 | Backwards facing step, Re_h = 5,000 | E | Jovic & Driver
chapter8\CMP32 Backwards facing step, Re_h = 37,500 | E | Driver & Seegmiller
LIST OF BINARY FILES
chapter3/HOM23/*.bin (5 files)
chapter3/HOM24/correlat/*.bin (15 files)
chapter7/TBL01/re300/*.bin (5 files)
chapter7/TBL01/re670/*.bin (5 files)
chapter7/TBL21/cor*.bin (9 files)
chapter8/CMP30/*.bin (7 files)
LIST OF PARTICIPANTS IN WG21
Carlo Benocci, VKI, Brussels.
Jean-Paul Bonnet, University of Poitiers.
Brian Cantwell, Stanford University.
Javier Jimenez (Chairman), Universidad Politecnica of Madrid.
Otto Leuchter, ONERA, Meudon.
Robert D. Moser, University of Illinois, Urbana.
L. Patrick Purtell, ONR, Arlington, Virginia.
Michelle Onorato, Politecnico of Torino.
Wolfgang Rodi, University of Karlsruhe.
Peter D. Smith, DERA, Farnborough.
Stavros Tavoularis, University of Ottawa.
Jaap J.W. van der Vegt, NLR, Amsterdam.