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Announcing TU Delft Repository replacement
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2 July 2024
TU Delft Repository will be replaced with a fresh user friendly design with monthly new feature releases.
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Boundary-layer calculations on the leeward surface of a slender delta wing at incidence
A system for computer aided analysis and design of multi-element airfoils
Application of computational procedures in aerodynamic design
A system for the numerical simulation of sub- and transonic viscous attached flows around wing-body configurations
Comparison of boundary layer calculations for the root section of a wing
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