You shouldn't worry about using code formulae. The fact that you are lacking the metal between the bolt holes doesn't change anything, as code formulae do not account for metal outside
d, the diameter of the sealing circle (not shown on your drawing).
This is easily proved, as the bending stress in a supported circular plate with uniform pressure is
[σ]=3(3+
[ν])
Pd2/32
t2 (where
d is the outer diameter of the plate) and this gives
C very close to 0.3. To be noted that
[ν] should be set to zero, as it gives rise to secondary stresses, and this makes the code formula a little conservative (
C=0.28). Also this means that the code formula doesn't account for an allowable stress in bending equal to 1.5
SE.
Concerning the bolt load, this gives a uniform bending stress in the plate equal to
[σ]=6
WhG/[π]
dt2 that gives exactly the formula in the code.
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