This screen is used to specify the spar and shear web details. The items on this screen are as follows;
This screen is used to specify the spar and shear web details. The items on this screen are as follows;
Number is automatically assigned by WINFOIL when a spar is created.
Units default to the units selected for the wing or tail design.
Type is the type of spar. This can be either of the following; leading edge, trailing edge or intermediate.
Root and Tip are the Root and Tip chord lengths respectively. These are expressed in the dimensional units selected for the wing or tail design.
Chord Position % is the location of the spar as a percentage of the root chord.
At Max. Thickness places the spar location at the position of maximum thickness based on the root airfoil selected. Click on this to position at this point. From a structural viewpoint the maximum thickness point is the ideal placement for an intermediate spar as spar strength is proportional to the vertical depth. The greater the depth the greater the bending strength.
Check Root/Tip Depths button. Click on this button to determine the depth at the root and tip at the chord position selected. If the depth of the spar exceeds these measurements then the spar depth will default to full depth.
Root Width is the width of the spar in units defined by the wing or tail design.
Depth is the depth of the spar at the root. Leading and trailing edge spars default to a depth of zero as these are full depth.
Web thickness is the thickness of the shear web. Intermediate spars have two shear webs. One on each facing side of the spar. Leading and trailing edge spars can only have one web on the inboard side of the spar. The units for the shear web are the same as for the wing or tail design.
Tip Depth is the depth of the spar at the tip. This is in the same units selected for the wing or tail design.
Click on the UPDATE button to update the data or click on the CLOSE button to exit without making any changes.
Tip Reducing the depth of the spar at the tip will reduce the weight of a cantilever wing without sacrificing strength as the bending moment at the tip is zero.