Add to ORKGA calculation method for the aerodynamic prediction of airfoils based on a new interactive boundary-layer approach and an improved Cebeci-Smith eddy viscosity formulation is described. Results are presented for airfoils at low and moderate Reynolds numbers in order to demonstrate the need to calculate transition for accurate drag polar and maximum lift coefficient prediction. 1
This work presents the analysis, application, and comparison of thirteen fluid flow models in the pr...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
The article describes procedure of sailplane airfoil optimization with use of available numerical an...
Abstract. A calculation method for the aerodynamic prediction of mul ielement airfoils based on an i...
Boundary layer calculations are performed around an airfoil and its wake. Smith-van Ingen transition...
To reduce drag on wings, aerodynamicists have long been trying to keep the boundary layer on the win...
Low Mach number viscous-inviscid interaction is considered using panel methods, direct and inverse b...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
A new airfoil performance software is developed by combining two independent codes . The first one i...
The article of record as published may be found at https://doi.org/The article of record as publishe...
A Computational method was developed for investigating boundary layer control. Solutions of the Reyn...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
When analyzing the flow over airfoils at relatively low Reynolds numbers, transition from laminar to...
This work presents the analysis, application, and comparison of thirteen fluid flow models in the pr...
An unstructured Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and a fully au...
This work presents the analysis, application, and comparison of thirteen fluid flow models in the pr...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
The article describes procedure of sailplane airfoil optimization with use of available numerical an...
Abstract. A calculation method for the aerodynamic prediction of mul ielement airfoils based on an i...
Boundary layer calculations are performed around an airfoil and its wake. Smith-van Ingen transition...
To reduce drag on wings, aerodynamicists have long been trying to keep the boundary layer on the win...
Low Mach number viscous-inviscid interaction is considered using panel methods, direct and inverse b...
The lift/drag ratio of an airfoil placed in an incompressible attached flow is maximized taking into...
A new airfoil performance software is developed by combining two independent codes . The first one i...
The article of record as published may be found at https://doi.org/The article of record as publishe...
A Computational method was developed for investigating boundary layer control. Solutions of the Reyn...
Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercia...
When analyzing the flow over airfoils at relatively low Reynolds numbers, transition from laminar to...
This work presents the analysis, application, and comparison of thirteen fluid flow models in the pr...
An unstructured Reynolds-averaged Navier-Stokes solver, a laminar boundary-layer code and a fully au...
This work presents the analysis, application, and comparison of thirteen fluid flow models in the pr...
A semi-inverse viscous/inviscid coupling technique for the calculation of compressible flows is pres...
The article describes procedure of sailplane airfoil optimization with use of available numerical an...