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Left end simply supported, right end simply supported for intermediate externally created lateral displacement
Values for calculation
Calculation
Vertical end reactions $ R_A $
$$R_A=0$$
$R_A=0$
Equations in LaTeX code
R_A=0
Reaction end moment $ M_A $
$$M_A=0$$
$M_A=0$
Equations in LaTeX code
M_A=0
Angular displacement $ θ_A $
$$θ_A=\cfrac{-Δ_o}{l}$$
$θ_A=\cfrac{-Δ_o}{l}$
Equations in LaTeX code
θ_A=\cfrac{-Δ_o}{l}
Deflection $ y_A $
$$y_A=0$$
$y_A=0$
Equations in LaTeX code
y_A=0
Vertical end reactions $ R_B $
$$R_B=0$$
$R_B=0$
Equations in LaTeX code
R_B=0
Reaction end moment $ M_B $
$$M_B=0$$
$M_B=0$
Equations in LaTeX code
M_B=0
Angular displacement $ θ_B $
$$θ_B=\cfrac{-Δ_o}{l}$$
$θ_B=\cfrac{-Δ_o}{l}$
Equations in LaTeX code
θ_B=\cfrac{-Δ_o}{l}
Deflection $ y_B $
$$y_B=0$$
$y_B=0$
Equations in LaTeX code
y_B=0
Max. deflection +
$$y_{max+}=\cfrac{Δ_o}{l}\cdot\left(l-a\right)$$
$y_{max+}=\cfrac{Δ_o}{l}\cdot\left(l-a\right)$
Equations in LaTeX code
y_{max+}=\cfrac{Δ_o}{l}\cdot\left(l-a\right)
Max. deflection -
$$y_{max-}=\cfrac{-Δ_o\cdot a}{l}$$
$y_{max-}=\cfrac{-Δ_o\cdot a}{l}$
Equations in LaTeX code