Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme
    
    
  
  
  
      
      
      
        
Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 4 (2015), pp. 65-68
    
  
  
  
  
  
    
      
      
        
      
      
      
    Voir la notice de l'article provenant de la source Math-Net.Ru
            
              			The paper considers some results of numerical simulation of flow around ONERA M6 profile. The solver is based on a fully implicit finite volume third order sheme for 3D Reynolds averaged Navie–Stockes equations with the Edwards modification of the Spalart–Allmaras turbulence model. The scalability of the parallel solver is analyzed. The numerical results are compared with experimental data and with the results obtained using an explicit scheme.
			
            
            
            
          
        
      @article{VMUMM_2015_4_a12,
     author = {V. E. Borisov},
     title = {Simulation of flow over the {ONERA} {M6} wing using a parallel implementation of an implicit scheme},
     journal = {Vestnik Moskovskogo universiteta. Matematika, mehanika},
     pages = {65--68},
     publisher = {mathdoc},
     number = {4},
     year = {2015},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMUMM_2015_4_a12/}
}
                      
                      
                    TY - JOUR AU - V. E. Borisov TI - Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme JO - Vestnik Moskovskogo universiteta. Matematika, mehanika PY - 2015 SP - 65 EP - 68 IS - 4 PB - mathdoc UR - http://geodesic.mathdoc.fr/item/VMUMM_2015_4_a12/ LA - ru ID - VMUMM_2015_4_a12 ER -
%0 Journal Article %A V. E. Borisov %T Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme %J Vestnik Moskovskogo universiteta. Matematika, mehanika %D 2015 %P 65-68 %N 4 %I mathdoc %U http://geodesic.mathdoc.fr/item/VMUMM_2015_4_a12/ %G ru %F VMUMM_2015_4_a12
V. E. Borisov. Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme. Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 4 (2015), pp. 65-68. http://geodesic.mathdoc.fr/item/VMUMM_2015_4_a12/
