Details
Verification and validation of computational fluid dynamics
In association with the Thematic Network FLOWNET (European Commission DG XII)
June 5 - 8, 2000; F. Grasso, J. Périaux, H. Deconinck
Table of content
- DENIAU, H.; LAMBALLAIS, E.; DELVILLE, J.; ALZIARY DE ROQUEFORT, T. - Laboratoire d'Etudes Aerodynamiques - UMR CNRS, France
Validation for turbulence modeling - DÉLERY, J. & CHANETZ, B. - ONERA, France
Experimental aspects of code verification/validation - Application to internal aerodynamics - PANDOLFI, M. & D'AMBROSIO, D. - Politecnico di Torino, Italy
Verification and validation: numerical issues - GARBEY, M. & TROMEUR DERVOUT, D. - ISTIL/University Lyon 1 Claude Bernard, France
Code verification in parallel computing environment
Toward a learning system in scientific computing - DÉSIDÉRI, J.-A.1 & PÉRIAUX, J.2 - INRIA1 & Dassault Aviation2, France
The role of databases for CFD validation
Part I: Validation of high-speed flow simulations by means of network data base - LESERVOISIER, D.1,2; CARTE, G.1; DERVIEUX, A.1 - INRIA1 & SNECMA2, France
The role of databases for CFD validation
Part II: High-order interpolation and mesh optimization for validated CFD - FARHAT, C.1; LESOINNE, M.1; KOOBUS, B.2,3 - CAS1, Université de Montpellier2, INRIA3, USA1 & France 2,3
The role of databases for CFD validation
Part III: An example testcase from the FLOWnet database: Flutter analysis of an AGARD Wing 445.6 - SCHWAMBORN, D. - DLR, Germany
Verification and validation: examples for a solver using hybrid unstructured grids - GRASSO, F.1; PÉRIAUX, J.2; DÉSIDÉRI, J.-A.3 - Univ. di Roma La Sapienza 1, Dassault Aviation 2, INRIA3, Italy1 & France2,3
The FLOWNET project: a flow library on the web - OBERKAMPF, W.L. - Sandia National Laboratories, USA
Introduction to verification and validation
Design, execution, and analysis of validation experiments
FLOWNET CASE STUDIES
- WEINERFELT, P. - SAAB, Sweden
TEST CASE SB04: High lift Navier-Stokes calculations and experimental data for the 2D NLR 7301 wing-flap geometry - BUR, R. & DÉLERY, J. - ONERA, France
TEST CASE TR03: 3-D transonic interaction on a swept bump - HENZE, A. - RWTH Aachen, Germany
TEST CASE SP06: Contribution to SP06: ELAC-I delta wing - ZEITOUN, D.E. - Université de Provence-IUSTI-UMR, France
Supersonic shock wave reflections in steady flows
Test Case SP 10 - FLOWNet database - DIEUDONNÉ, W.; BOERRIGTER, H.L.; CHARBONNIER, J.-M. - von Karman Institute, Belgium
Test Case H05 - Hypersonic flow on a blunted cone-flare and in the VKI-H3
Mach 6 wind tunnel - ARTS, T. - von Karman Institute, Belgium
TEST CASE TU02: Aero-thermal performance of a high pressure turbine nozzle guide vane - KANG, S.; LACOR, C.; HIRSCH, C. - VUB, Belgium
TEST CASE W01: Simulation of the flow through the NREL windturbine (W01) - HAASE, W. - Daimler Chrysler Aerospace, Germany
Test Case MO - Two-point Airfoil Optimization - SCHWAMBORN, D. - DLR, Germany
TEST CASE: UF03 The Oscillating Delta Wing - CELLI, M; FANION, T.; ROGE, G. - Dassault Aviation, France
TEST CASE MF02: Flutter analysis of an AGARD 445.6 wing
Additional Information
Manufacturer | von Karman Institute for Fluid Dynamics |
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