configuration block
1.Four turbulence models:algebraic Baldwin?Lomax model with Degani?Schiff modification, two versions of Johnson?King model (J?K90A and J?K92) and two?equation ?k?g? model, are described and evaluated for missile supersonic flow, NASA TN D?712 standard model and the civil airplane wing?body configuration (two?block C?O mesh) transonic flows.
2.Results 4 analyzed criteria had a specificity of 97%, 98%, 94%,93% a triphasic configuration (Rsr′,rSR′,RSR′) QRS complex in V 1 with right bundle branch block morphology (BBBM);
