MSES/MISES |
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Whether you need a single airfoil section, multiple sections for a highlift system, or an airfoil for a cascade, this suite of codes allows you to quickly translate your design requirements into an optimum configuration.
Two-dimensional codes driven with X-Window GUIs allow rapid geometry changes, parametric flow studies, and configuration development; MSES for multi-element airfoils in subsonic and transonic flow; MISES for airfoils in a transonic cascade.
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MSES streamline grid for a 3 - element Formula 1 rear wing
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MISES solution for DFVLR transonic
compressor cascade at M=0.82
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Both codes offer inverse design, forced and natural transition, and direct and inverse interactive boundary layer methods. Grid generation is automatic using a streamline coordinate solution, allowing the grid to adapt to the evolving flow field.
There is no better way to achieve your ideal airfoil design in the least possible time.
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System Requirements |
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This software is available for the following systems: aix,hpux(PA-RISC),irix,linux,osf (MSES also available for sun)
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Additional Information |
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