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$σ_{e_{test}}=\cfrac{R_{p0.2/T_{test}}}{1.25}$
Equations in LaTeX code
σ_{e_{test}}=\cfrac{R_{p0.2/T_{test}}}{1.25}
$\text{else}$
$\text{else}$
Equations in LaTeX code
\text{else}
$$σ_{e_{test}}=R_{p0.2/T_{test}}$$
$σ_{e_{test}}=R_{p0.2/T_{test}}$
Equations in LaTeX code
σ_{e_{test}}=R_{p0.2/T_{test}}
Pressure at which mean circumferential stress in cylindrical or conical shell midway between stiffeners, or in a spherical shell, reaches yield point for normal operating load cases
$$P_y=\cfrac{σ_e\cdot e_a}{R}$$
$P_y=\cfrac{σ_e\cdot e_a}{R}$
Equations in LaTeX code
P_y=\cfrac{σ_e\cdot e_a}{R}
Pressure at which mean circumferential stress in cylindrical or conical shell midway between stiffeners, or in a spherical shell, reaches yield point for testing load cases
$$P_{y_{test}}=\cfrac{σ_{e_{test}}\cdot e_a}{R}$$
$P_{y_{test}}=\cfrac{σ_{e_{test}}\cdot e_a}{R}$
Equations in LaTeX code
P_{y_{test}}=\cfrac{σ_{e_{test}}\cdot e_a}{R}
Parameter $ Z $
$$Z=\cfrac{π\cdot R}{L}$$
$Z=\cfrac{π\cdot R}{L}$
Equations in LaTeX code
Z=\cfrac{π\cdot R}{L}
Number of circumferential waves for an unstiffened part of a cylinder