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The sort of cross section that is adopted for the wings of aircraft has been sketched already in Figure 17B.
Red marks, area of cross section.
Area of cross section of the cylinder.
The analysis of cross section would help clarify this question.
Bending moment resistance of cross section and of member (column).
Black line denotes the location of cross section.
Similar(31)
Dotted line indicates position of cross-section.
Two types of cross-section channel geometries were used.
The shapes of cross-section of all fibers are round.
Effects of cross-section flattening, local transverse effects, support rotation and the effects of cross-section compactness on the overall behaviour of the blast barriers are discussed.
A subsequent parametric study was carried out, considering a range of cross-section and member geometries.
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