Load type > Mean drag for longitudinal wind component

Definition of a wind loading along the element axis. (Drag force q = cd * Rho * v^2 / 2)

Setting	Description
From, To, Step	Element series to be loaded
Assembly	Alternative to load assignment via element series: Name of the assembly to be loaded. The specified load is applied to every element of the specified assembly.
Rho	Air density (tons per volume unit) Note: No default value. The density must be explicitly specified. (Value appr. 0.00125 t/m^3; mass unit always tons t, cannot be changed)
v-beg	Wind velocity at element begin
v-end	Wind velocity at element end Note: The load intensity q = cd * Rho * v^2 / 2 is calculated for the element begin and element end, and then applied as trapezoidal load
cd	Drag coefficient
Options: None, Mult. by CS width, Mult. by CS depth	None: Area included in the drag coefficient (q = cd * Rho * v^2 / 2) Mult. By CS width: Drag coefficient related to the cross-section width b (q = cd * b * Rho * v^2 / 2) Mult. By CS depth: Drag coefficient related to the cross-section depth h (q = cd * h * Rho * v^2 / 2)
[OK+Series]	To continue with further input of the same load type