I. Equivalent stress (σ c) is calculated by the following formula or another formula specially approved by the Commandant (CG-522) as equivalent to the following:

eCFR graphic ec02fe91.090.gif

where:

σx = total normal stress in “x” direction.

σy = total normal stress in “y” direction.

τxy = total shear stress in “xy” plane.

II. When the static and dynamic stresses are calculated separately, the total stresses in paragraph I are calculated from the following formulae or another formulae specially approved by the Commandant (CG-522) as equivalent to the following:

eCFR graphic ec02fe91.091.gif

eCFR graphic ec02fe91.092.gif

eCFR graphic ec02fe91.093.gif

III. Each dynamic and static stress is determined from its acceleration component and its hull strain component from hull deflection and torsion.

[CGD 74-289, 44 FR 26009, May 3, 1979, as amended by CGD 82-063b, 48 FR 4782, Feb. 3, 1983]


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