Contract No: AST5-CT-2006-030959

WORKSHOP on QUANTIFICATION of CFD UNCERTAINTIES

29-30 October 2009
Vrije Universiteit Brussel
Brussels, BELGIUM

Workshop’s objectives

  • To assess non-deterministic methodologies on compulsory test cases
  • To promote and stimulate the development and application of the non-deterministic methodologies
  • To review the state of the art by renowned keynote speakers
  • To present the developments and results of the NODESIM- CFD consortium


Academics and professionals from aeronautical community are encouraged to participate in this workshop with contributions directed to one of the workshop’s objectives. in addition to paper contributions, participants are expected to contribute nondeterministic simulation results, concerning at least one of the two compulsory test cases selected by the organizers.


TEST CASE 1

The first test case is the transonic flow around the RAE 2822 airfoil at Mach number M=0.734; angle of incidence 2.79 deg and Reynolds number Re= 6.5x10^6.
Uncertainties are imposed on the angle of incidence, the thickness-to-chord ratio and the Mach number.

Contributors are expected to deal both with the case where these uncertainties have a uniform distribution and the case where they have a normal distribution.

The required outputs are the probability density functions, mean and standard deviations for: drag; lift and moment coefficients. Analysis should be based on a RANS solver.

Click here for the full test case description


TEST CASE 2

The second test case is the flow in the transonic axial compressor, known as NASA Rotor 37.
Uncertainties are imposed on the inlet total pressure, the static outlet pressure and the tip clearance.

 

Uncertain
parameter

The most likely value (m)

Minimum value (a)

Maximum value (b)

PDF type

1

Inlet total pressure

Experimental input profiles (m)

95% m

105% m

Beta pdf

2

Static outlet pressure

mp=1.1 bar

98% mp

102%mp

Beta pdf

3

Tip clearance

mH=0.356 mm

50% mH

150%mH

Beta pdf

_part1.png

The computed results will be represented as bar plots on profiles of the pressure ratio, isentropic efficiency and total temperature ratio versus mass flow.

Click here for the full test case description


Workshop’s deadlines

Submission of abstracts
Abstracts of maximum 1000 words should be submitted by 1st of September 2009 to cristian.dinescu@numeca.be.

Notification
The notifications of acceptance will be sent to the authors by 10th of September 2009.

Submission of workshop’s results on test cases and papers
The computational results related to the compulsory test cases and the papers must be submitted to cristian.dinescu@numeca.be no later than 21st of September 2009.

Registration
The attendees must register by 28th of September 2009. The registration fee is 150 euros.

Click here for the REGISTRATION form.

Official language
The official language of the workshop is English.

Organizing Committee
Chairman: Charles Hirsch (charles.hirsch@numeca.be)

Secretary: Cristian Dinescu (cristian.dinescu@numeca.be)

Members

Hester Bijl
H.Bijl@tudelft.nl

Gabriel Budega
budega@cimne.upc.edu

Vincent Couaillier
Vincent.Couaillier@onera.fr

Alain Dervieux
Alain.Dervieux@inria.fr

Chris Lacor
chris.lacor@vub.ac.be

Gilbert Roge
Gilbert.Roge@dassault-aviation.com

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