1st International Workshop on High-Order CFD Methods
Sponsored
by Fluid Dynamics TC, AFOSR and DLR
January 7-8, 2012
at the 50th AIAA Aerospace Sciences Meeting, Nashville,
Tennessee
Objectives
General Information
Important Dates
, Jan. 30, 2011 - Test
cases defined with most geometries available
, Feb. 28, 2011 -
E-mail
hiocfd@gmail.com for your intention to
participate (for planning purpose)
, March 1, 2011 - Grids
available for some cases
, Oct. 15, 2011 - Abstract
(abstract template) and fellowship
application with an endorsement letter from the advisor (abstract needed to
present your work). Do send an incomplete abstract if you believe data will be
ready on Nov. 15th.
, Nov. 1, 2011 - Acceptance
e-mail sent out
, Nov. 15, 2011 - Data
submittal
, Jan. 7-8, 2012 - Workshop
(registration required to participate)
List of
Accepted Abstracts (10/17/11)
Preliminary
Agenda (01/04/2012)
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New! Workshop Results (Some errors in
the summary are being corrected!!!)
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Important Guideline
(Read this first!)
Notes for all participants. If you have any
questions, send e-mail to: hiocfd@gmail.com
Follow
http://twitter.com/#!/hiocfd for
updates!
Test Cases
C1. Easy, 2D
C1.1 Internal
inviscid flow over a smooth bump (Abgrall)
(1/30/11), Mixed order and
uniform order grids (5/24/11)
C1.2 Transonic
Ringleb flow (Huynh) (1/30/11), p4 quad grids (8/25/11)
C1.3 Flow
over the NACA0012 airfoil, inviscid and viscous, subsonic and transonic
(May), p4 quad & triangular grids (far
field boundary over 1000 chords away) (8/3/11).
C1.4 Flat
plate boundary layer (Bassi) (1/30/11), quad grids
(9/23/11)
C1.5 Radial
expansion wave (van Leer) (Attention added on 9/30/11)
C1.6 Vortex
transport by uniform flow (Caraeni) (Updated on 10/05/11), Grids (4/11/11)
C2. Intermediate, 2D
& 3D
C2.1 Unsteady
viscous flow over tandem NACA0012 airfoils with a smooth initial condition
(Cary) (1/30/11)
C2.2 Turbulent
flow over a RAE airfoil (Deconinck), Linear and
higher order grids (5/24/11)
C2.3 Analytical
3D body of revolution (Kroll), Linear and high-order
grids (5/24/11)
C2.4 Delta
wing at low Reynolds number (Hartmann) Grids
(updated 8/15/11)
C3. Difficult, 2D &
3D
C3.1 Turbulent
flow over a multi-element airfoil (Wang) (1/30/11), Geometry (5/11/11)
C3.2 Turbulent
flow over DPW III wing alone (Fidkowski) (1/30/11), Grids
(9/8/11)
C3.3 Transitional
flow over a SD7003 wing (Visbal) (1/30/11), Geometry posted on 5/11/11 (Points or IGES
file)
C3.4 2D
laminar flapping wing case (Persson) (1/30/11)
C3.5 Direct
Numerical Simulation of the Taylor-Green Vortex at Re = 1600 (Hillewaert)
(4/18/11), reference data (8/24/11)
Organizing Committee
,
Remi
Abgrall, INRIA and University of Bordeaux
,
Francesco
Bassi, University of Bergamo
,
Doru Caraeni,
CD-adapco
,
Andrew
Cary, Boeing
,
Herman
Deconinck, VKI
,
Chris
Fidkowski, University of Michigan
,
Ralf
Hartmann, DLR
,
Koen
Hillewaert, CENAERO
,
H.T.
Huynh, NASA Glenn Research Center
,
Norbert
Kroll (Co-Chair), DLR
,
Georg
May, RWTH Aachen University
,
Per-Olof
Persson, UC Berkeley
,
Bram
van Leer, University of Michigan
,
Miguel
Visbal, AFRL
,
Z.J.
Wang (Co-Chair), Iowa State University
For up-to-date information, visit the workshop website:
http://www.cfdc.iastate.edu/hiocfd
or email hiocfd@gmail.com