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Boundary integral method for the computation of the potential flow about ship configurations with lift and free surface effects
Boundary integral method for the computation of the potential flow about ship configurations with lift and free surface effects
On wings and keels (II)
On wings and keels (II)
Design of transonic airfoils with given pressure, subject to geometric constraints
Design of transonic airfoils with given pressure, subject to geometric constraints
Inverse method with geometric constraints for transonic airfoil design
Inverse method with geometric constraints for transonic airfoil design
A survey of computational methods for subsonic and transonic aerodynamic design
A survey of computational methods for subsonic and transonic aerodynamic design
On wings and keels
On wings and keels
Application of computational procedures in aerodynamic design
Application of computational procedures in aerodynamic design
Computational methods for subsonic and transonic aerodynamic design
Computational methods for subsonic and transonic aerodynamic design
A comparison of computational and experimental results for the transonic flow around the DFVLR-F4 wing-body configuration
A comparison of computational and experimental results for the transonic flow around the DFVLR-F4 wing-body configuration
Some new developments in exact integral equation formulations for sub- or transonic potential flow
Some new developments in exact integral equation formulations for sub- or transonic potential flow
A system for the numerical simulation of sub- and transonic viscous attached flows around wing-body configurations
A system for the numerical simulation of sub- and transonic viscous attached flows around wing-body configurations
Requirements and developments shaping a next generation of integral methods
Requirements and developments shaping a next generation of integral methods
A constrained inverse method for the aerodynamic design of thick wings with given pressure distribution in subsonic flow
A constrained inverse method for the aerodynamic design of thick wings with given pressure distribution in subsonic flow
Inventarisatie van wensen t.a.v. computerfaciliteiten voor aërodynamische berekeningen in de tachtiger jaren
Inventarisatie van wensen t.a.v. computerfaciliteiten voor aërodynamische berekeningen in de tachtiger jaren
Calculation of transonic flow by means of a shock-capturing field panel method
Calculation of transonic flow by means of a shock-capturing field panel method
Calculation of transonic flow by means of a shock-capturing field panel method
Calculation of transonic flow by means of a shock-capturing field panel method
Conclusies van enkele oriënterende studies voor een rekenmethode voor drie-dimensionele transsone potentiaal stromingen om romp-vleugel configuraties
Conclusies van enkele oriënterende studies voor een rekenmethode voor drie-dimensionele transsone potentiaal stromingen om romp-vleugel configuraties
Aerodynamic design of thick, supercritical wings through the concept of equivalent subsonic pressure distribution
Aerodynamic design of thick, supercritical wings through the concept of equivalent subsonic pressure distribution
Wind tunnel tests and aerodynamic computations: Thoughts on their use in aerodynamic design
Wind tunnel tests and aerodynamic computations: Thoughts on their use in aerodynamic design
Remarks on the suitability of various transonic small perturbation equations to describe three-dimensional transonic flow; examples of computations using a fully-conservative rotated difference scheme
Remarks on the suitability of various transonic small perturbation equations to describe three-dimensional transonic flow; examples of computations using a fully-conservative rotated difference scheme
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