In Excel I typed drawing stress formula as:
σy * (3.2/( Δ + 0.9)) (α+ μ) = 572,776
σy * ((3.2/ Δ ) + 0.9) (α+ μ) = 51,760
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Draw Stress
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51,760
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$B$31 * (3.2/$B$21) + 0.9) * ($B$13+ $B$25)
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200,000 * 1.312 * .1972
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Pounds Force
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Draw Stress * Area
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51,760 * 3.799
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Draw Force
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196,657 lb
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=$B$40 * $B$17
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Thanks, you were right about the error.
I have the updated 14A now, thanks Scott Henry.
Can I use the actual Yield as the Average flow stress?
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David Kirchner
COO
High Performance Alloys, Inc
Tipton IN
(765) 945-8230
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Original Message:
Sent: 12-15-2023 13:36
From: David Coulston
Subject: Draw Bench math
David,
I am a little bit confused by this calculation:
| σy * (3.2/ Δ ) + 0.9) (α+ μ) |
I am probably not grabbing the right numbers... but when I plug values in, I get an answer that is about 1/10 of the 572,776 value you ended up with.
Another Dave
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David Coulston
Niles MI
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