Numerical simulation of leading-edge vortex flow

Computational aerodynamics of ordered vortex flows

Panel methods in aerodynamics: Some highlights

Computation of three-dimensional boundary layer transition and separation on a 65deg swept delta wing at 20deg angle of attack

Numerical simulation of vortical flow

Modeling of time-variant flows using Vortex dynamics-activities in the Netherlands

A method for computing the three—dimensional flow about wings with leading—edge vortex separation Part II: Description of computer program VORSEP

Theoretical and experimental investigations into Vortex flow

An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application

An approximate method for computing inviscid vortex wake roll-up. Part II. Description of computer program vor2DT

Vortex-fitted potential solution compared with cortex-captured Euler solution for delta wing with leading-edge vortex separation

Methods for numerical simulation of leading-edge vortex flow

Numerical computation of vortical flow about wings

Computational vortex flow aerodynamics

A panel method for the prediction of aerodynamic characteristics of complex configurations in linearized subsonic of supersonic flow

On the vortex flow over delta and double-delta wings

A higher order panel method applied to Vortex sheet roll-up

A Higher-order panel method for the computation of the flow about slender delta wings with leading-edge vortex separation

Aspects of second- and third-order panel methods demonstrated for the two-dimensional flat plate problem

A panel method for the determination of the aerodynamic characteristics of complex configurations in linearized subsonic or supersonic flow. Part 3. Description of computer code NLRAERO