Add to ORKGA lower-upper symmetric Gauss-Seidel (LU-SGS) subiteration scheme is constructed for time-marching of the fluid equations. The Harten-Lax-van Leer-Einfeldt-Wada (HLLEW) scheme is used for the spatial discretization. The same subiteration formulation is applied directly to the structural equations of motion in generalized coordinates. Through subiteration between the fluid and structural equations, a fully implicit aeroelastic solver is obtained for the numerical simulation of fluid/structure interaction. To improve the ability for application to complex configurations, a multiblock grid is used for the flow field calculation and transfinite interpolation (TFI) is employed for the adaptive moving grid deformation. The infinite plate spline (...
In the last two decades there have been extensive developments in computational unsteady transonic a...
The current status of computational methods for unsteady aerodynamics and aeroelasticity is reviewed...
The maturity of simulation codes for aerodynamics (CFD) and structures (CSD) now leads to high fidel...
Through the coupling between aerodynamic and structural governing equations, a fully implicit multib...
Abstract Through the coupling between aerodynamic and structural governing equations, a fully implic...
The design of a large aircraft at high speeds is a challenge in the very active research on aeroelas...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
The maturity of simulation codes for aerodynamics (CFD) and structures (CSD) now leads to high fidel...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
The exploitation of computational fluid dynamics for non linear aeroelastic simulations is mainly ba...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
In the last two decades there have been extensive developments in computational unsteady transonic a...
The current status of computational methods for unsteady aerodynamics and aeroelasticity is reviewed...
The maturity of simulation codes for aerodynamics (CFD) and structures (CSD) now leads to high fidel...
Through the coupling between aerodynamic and structural governing equations, a fully implicit multib...
Abstract Through the coupling between aerodynamic and structural governing equations, a fully implic...
The design of a large aircraft at high speeds is a challenge in the very active research on aeroelas...
Research in the area of computational unsteady transonic flows about airfoils and wings, including a...
Research in the area of computational, unsteady transonic flows about airfoils and wings, including ...
The maturity of simulation codes for aerodynamics (CFD) and structures (CSD) now leads to high fidel...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
The exploitation of computational fluid dynamics for non linear aeroelastic simulations is mainly ba...
Current research efforts in aeroelasticity aim at including higher fidelity aerodynamic results into...
In the last two decades there have been extensive developments in computational unsteady transonic a...
The current status of computational methods for unsteady aerodynamics and aeroelasticity is reviewed...
The maturity of simulation codes for aerodynamics (CFD) and structures (CSD) now leads to high fidel...