Porous airfoil and process

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244204, B64C 2102

Patent

active

051673878

ABSTRACT:
A porous airfoil having venting cavities with contoured barrier walls, formed by a core piece, placed beneath a porous upper and lower surface area that stretches over the nominal chord of an airfoil is employed, to provide an airfoil configuration that becomes self-adaptive to very dissimilar flow conditions to thereby improve the lift and drag characteristics of the airfoil at both subcritical and supercritical conditions.

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