Add to ORKGThin layer Navier-Stokes and Euler equations are numerically solved using a multi-block zonal approach to simulate the formation and roll up of tip vortices of wings in subsonic and transonic flows. Several wing planforms were considered to examine the influence of tip-cap shape, planform geometry and free stream Mach number on the formation process. A good definition of the formation and qualitative roll up of tip vortices was achieved
Wing tip vortices, and their relationship to wing tip geometry and wing total drag, are investigate...
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
The viscous transonic flow around a low aspect ratio wing was computed by an implicit, three dimensi...
Vortex flows caused by a swept wing are described in some detail. The thin-shear-layer Navier-Stokes...
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition meth...
A high resolution computational methodology is developed for the solution of the Compressible Reyno...
In this study numerical calculations are conducted to understand implementation of different wingtip...
The tip vortex flowfield plays a significant role in the performance of advanced aircraft propellers...
Computational fluid dynamics has an increasingly important role in the design and analysis of aircra...
The current experimental study investigates the details of the formation, structure, and development...
Flow-angle and pressure surveys behind five, thin, pointed-tip wings of varying plan form have been ...
Wingtip vortices are generated by lifting airfoils; their salient features are compactness and relat...
Abstract: The current experimental study investigates the details of the formation, structure, and d...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
Wing tip vortices, and their relationship to wing tip geometry and wing total drag, are investigate...
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
The viscous transonic flow around a low aspect ratio wing was computed by an implicit, three dimensi...
Vortex flows caused by a swept wing are described in some detail. The thin-shear-layer Navier-Stokes...
The thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition meth...
A high resolution computational methodology is developed for the solution of the Compressible Reyno...
In this study numerical calculations are conducted to understand implementation of different wingtip...
The tip vortex flowfield plays a significant role in the performance of advanced aircraft propellers...
Computational fluid dynamics has an increasingly important role in the design and analysis of aircra...
The current experimental study investigates the details of the formation, structure, and development...
Flow-angle and pressure surveys behind five, thin, pointed-tip wings of varying plan form have been ...
Wingtip vortices are generated by lifting airfoils; their salient features are compactness and relat...
Abstract: The current experimental study investigates the details of the formation, structure, and d...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
Wing tip vortices, and their relationship to wing tip geometry and wing total drag, are investigate...
Theoretical analysis and associated computer programs were developed for predicting properties of tr...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...