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Clebsch variable model for unsteady inviscid transonic flow with strong shock waves
Development of an advanced panel method for complex configurations in subsonic compressible flow; Application to the computation of the potential flow through ducts.
ARSPNSC: A method to calculate subsonic steady and unsteady potential flow about complex configurations
A method for computing the three—dimensional flow about wings with leading—edge vortex separation Part II: Description of computer program VORSEP
An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application
A multigrid algorithm for steady transonic potential flows around aerofoils using Newton iteration
Aspects of second- and third-order panel methods demonstrated for the two-dimensional flat plate problem
A calculation method of the viscous flow around multi-component airfoils
Modified version of LTRAN2; a calculation method for inviscid transonic flow about thin airfoils in moderately slow unsteady motion
Application of the NLR Panel Method to a swept-wing/body combination with part-span flaps at low speed and comparison with experimental results
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