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NACA Symmetric Airfoil Equations by Ikram Bachtiar is a document available to read on EtoBox.
What is NACA Symmetric Airfoil Equations about?
The document presents universal equations for defining the shape of continuously variable symmetric NACA airfoils. It derives equations to determine the coefficients used in parametric equations that define the airfoil shape. The coefficients are determined based on control parameters like chord length, thickness location, and thickness. The final equations allow defining an airfoil shape within a CAD program by substituting the control parameters.
- Author
- Ikram Bachtiar
- Language
- EN