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Volumn 1, Issue , 2012, Pages 641-654

The Onera elsA CFD software: Input from research and feedback from industry

Author keywords

Aerodynamics; Aircraft; Helicopter; Navier Stokes; Turbomachinery

Indexed keywords

CFD SOFTWARES; CONTINUOUS IMPROVEMENTS; MULTI-PHYSICS; NAVIER STOKES;

EID: 84878609974     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (19)
  • 1
    • 85088183530 scopus 로고    scopus 로고
    • elsA an efficient Object-Oriented solution to CFD complexity
    • AIAA Paper 2002-0108
    • Cambier L and Gazaix M. elsA: an efficient Object-Oriented solution to CFD complexity. 40th AIAAASM, Reno, AIAA Paper 2002-0108, 2002.
    • (2002) 40th AIAAASM, Reno
    • Cambier, L.1    Gazaix, M.2
  • 2
    • 33748463335 scopus 로고    scopus 로고
    • The elsA Object-Oriented tool for industrial applications
    • Toronto
    • Gazaix M., Jollès A and Lazareff M. The elsA Object-Oriented tool for industrial applications. 23rd ICAS meeting, Toronto, 2002.
    • (2002) 23rd ICAS meeting
    • Gazaix, M.1    Jollès, A.2    Lazareff, M.3
  • 3
    • 77956250258 scopus 로고    scopus 로고
    • Status of the elsA Software for Flow Simulation and Multi-Disciplinary Applications
    • Reno, AIAA Paper 2008-0664
    • Cambier L. and Veuillot J.P. Status of the elsA Software for Flow Simulation and Multi-Disciplinary Applications. 46th AIAA ASM, Reno, AIAA Paper 2008-0664, 2008.
    • (2008) 46th AIAA ASM
    • Cambier, L.1    Veuillot, J.P.2
  • 6
    • 84878592439 scopus 로고    scopus 로고
    • Investigation of the laminar separation-induced transition with the γ-Reθt transition model on one very high-lift low-pressure turbine (T2) and one engine-like scale low-pressure turbine (TX) rotor blades at steady conditions and freestream turbulence
    • Paris
    • Babajee J., Arts T. Investigation of the laminar separation-induced transition with the γ-Reθt transition model on one very high-lift low-pressure turbine (T2) and one engine-like scale low-pressure turbine (TX) rotor blades at steady conditions and freestream turbulence. 47th 3AF Int. Symp. of Applied Aerodynamics, Paris, 2012.
    • (2012) 47th 3AF Int. Symp. of Applied Aerodynamics
    • Babajee, J.1    Arts, T.2
  • 7
    • 84915771509 scopus 로고    scopus 로고
    • Unsteady stator-rotor interaction coupled with exhaust hood effect for last stage steam turbines
    • Istanbul
    • Stanciu M., Fendler Y. and Dorey J.M. Unsteady stator-rotor interaction coupled with exhaust hood effect for last stage steam turbines. 9th European Turbomachinery Conf., Istanbul, 2011.
    • (2011) 9th European Turbomachinery Conf.
    • Stanciu, M.1    Fendler, Y.2    Dorey, J.M.3
  • 8
    • 84879806611 scopus 로고    scopus 로고
    • A Python module for Chimera assembly
    • NASA Ames, MoffettField, 2010
    • Ṕron S. and Benoit C. A Python module for Chimera assembly. 10th Overset Grid Symposium, http://www.onera.fr/dsna/cassiopee/images/2010-09-OversetGridConnector.pdf, NASA Ames, MoffettField, 2010.
    • 10th Overset Grid Symposium,
    • Ṕron, S.1    Benoit, C.2
  • 10
    • 84878578683 scopus 로고    scopus 로고
    • Random flow generation technique for civil aircraft jet simulations with the ZDES approach
    • Beijing
    • Brunet V. Random flow generation technique for civil aircraft jet simulations with the ZDES approach. 4th Symp. on Hybrid RANS-LES methods, Beijing, 2011.
    • (2011) 4th Symp on Hybrid RANS-LES methods
    • Brunet, V.1
  • 12
    • 84878565654 scopus 로고    scopus 로고
    • elsA-Hybrid: an all-in-one structured / unstructured solver for the simulation of internal and external flows Application to turbomachinery
    • Saint-Petersburg
    • De la Llave Plata M., Couaillier V., Le Pape M.C., Marmignon C. elsA-Hybrid: an all-in-one structured / unstructured solver for the simulation of internal and external flows Application to turbomachinery. 4thEUCASS Conf., Saint-Petersburg, 2011.
    • (2011) 4thEUCASS Conf.
    • De la Llave Plata, M.1    Couaillier, V.2    Le Pape, M.C.3    Marmignon, C.4
  • 14
    • 84857265360 scopus 로고    scopus 로고
    • Multiblock residual-based compact schemes for the computation of complex turbomachinery flows
    • Michel B., Cinnella P. and Lerat A., Multiblock residual-based compact schemes for the computation of complex turbomachinery flows. IJESMS, Vol. 3, Nos. 1/2, pp. 2-15, 2011.
    • (2011) IJESMS , vol.3 , Issue.1-2 , pp. 2-15
    • Michel, B.1    Cinnella, P.2    Lerat, A.3
  • 15
  • 18
    • 84878607009 scopus 로고    scopus 로고
    • Aeroelastic capabilities of the elsA solver for rotating machines applications
    • Paris
    • Dugeai A., Mauffrey M. and Sicot F. Aeroelastic capabilities of the elsA solver for rotating machines applications. IFASD, Paris, 2011.
    • (2011) IFASD
    • Dugeai, A.1    Mauffrey, M.2    Sicot, F.3
  • 19
    • 84878554661 scopus 로고    scopus 로고
    • Prediction of the aerodynamic effect of model deformation during transonic wind tunnel tests
    • Paris
    • Mouton S., Lyonnet M. and Le Sant Y. Prediction of the aerodynamic effect of model deformation during transonic wind tunnel tests. 47th 3AF Int. Symp. of Applied Aerodynamics, Paris, 2012.
    • (2012) 47th 3AF Int. Symp. of Applied Aerodynamics
    • Mouton, S.1    Lyonnet, M.2    Le Sant, Y.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.