formula_5_3a
codes.eurocode.en_1992_1_1_2004.chapter_5_structural_analysis.formula_5_3a
Formula 5.3a from EN 1992-1-1:2004: Chapter 5 - Structural Analysis.
Classes:
-
Form5Dot3aTransverseForceUnbracedMembers–Class representing formula 5.3a for the calculation of the transverse force for unbraced members, [\(H_{i}\)].
codes.eurocode.en_1992_1_1_2004.chapter_5_structural_analysis.formula_5_3a.Form5Dot3aTransverseForceUnbracedMembers
Form5Dot3aTransverseForceUnbracedMembers(
theta_i: DIMENSIONLESS, n_axial_force: KN
)
Bases: Formula
Class representing formula 5.3a for the calculation of the transverse force for unbraced members, [\(H_{i}\)].
See Figure 5.1 a1.
[\(H_{i}\)] Transverse force for unbraced members [\(kN\)].
EN 1992-1-1:2004 art.5.2(7) - Formula (5.3a)
Parameters:
-
theta_i(DIMENSIONLESS) –[\(\Theta_{i}\)] Eccentricity, initial inclination imperfections [-].
Use your own implementation of this value or use the :class:
Form5Dot1Imperfectionsclass. -
n_axial_force(KN) –[\(N\)] Axial force [\(kN\)].
Positive values for compression, tension is not allowed.
Notes
Eccentricity is suitable for statically determinate members, whereas transverse load can be used for both determinate and indeterminate members. The force [\(H_{i}\)] may be substituted by some other equivalent transverse action.
Source code in blueprints/codes/eurocode/en_1992_1_1_2004/chapter_5_structural_analysis/formula_5_3a.py
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codes.eurocode.en_1992_1_1_2004.chapter_5_structural_analysis.formula_5_3a.Form5Dot3aTransverseForceUnbracedMembers.latex
latex(n: int = 3) -> LatexFormula
Returns LatexFormula object for formula 5.3a.
Source code in blueprints/codes/eurocode/en_1992_1_1_2004/chapter_5_structural_analysis/formula_5_3a.py
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