Aero Handbook: Difference between revisions
From GTMS
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===General Sub-Aero terms=== | ===General Sub-Aero terms=== | ||
;Airfoil | ;Airfoil | ||
:The cross-sectional shape of a wing which generates a pressure differential on either side. | :The cross-sectional shape of a wing which generates a pressure differential on either side. | ||
;Biplane | |||
:An airfoil or system of airfoils above the main airfoil system in a wing. | |||
;Camber | |||
:The curvature of an airfoil. | |||
;Chord Length | |||
:The distance from the LE to the TE of an airfoil. | |||
;Free Stream | |||
:The state of air infinitely ahead of a given aerodynamic system such that it is not affected by the system. | |||
;Leading Edge (LE) | |||
:The front edge of an airfoil. | |||
;Mainplane | |||
:The first, primary airfoil in a system/series of airfoils. | |||
;Ply | |||
:A layer of fiber in a composite material. | |||
;Ply Schedule | |||
:The construction of a composite skin as defined by individual plys. | |||
;Sandwich Panel | |||
:A composite board made of fibers on either end of a core material. | |||
;Secondary | |||
:The airfoil immediately preceding the mainplane. | |||
;Span Length | |||
:The length of an airfoil along its width (perpendicular its chord). | |||
;Tertiary | |||
:The airfoil immediately preceding the secondary airfoil. | |||
;Trailing Edge (TE) | |||
:The rear edge of an airfoil. | |||
;Up/Down/In/Out Wash | |||
:The movement of air in a respective direction. | |||
;Yaw | |||
:The crosswind experienced by the system, represented by an angle <br>'''or'''<br> the angular difference in the car’s velocity and wind speed brought on by rotation through a corner. | |||
;Core | |||
:The central section of sandwich panel; usually a honeycomb-shaped material or foam. | |||
=Design Methods= | =Design Methods= | ||