IMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION, FOR DESIGNING THE EXTERNAL GEOMETRY OF AN AIRCRAFT AIRFOIL
The present disclosure belongs to the field of configuring the shape or geometry of an aircraft airfoil (1.1 - 1.7). In particular, the present invention provides a method to design the external geometry of an aircraft airfoil.
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | The present disclosure belongs to the field of configuring the shape or geometry of an aircraft airfoil (1.1 - 1.7). In particular, the present invention provides a method to design the external geometry of an aircraft airfoil. |
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