Ron, I am not surprised that Richard was a little confused by the two figures you used, I was also. I did a little digging and may have solved the mystery. BTW I checked your figures and they worked fine in relation to my more rudimentary methods. That is, your methods are suitably accurate but a little confusing to those less versed in engineering. Finding the angle as you did really stumped me, I would usually rely on the more conventional formula. The sin of halve the angle = ½ the rib length divided be the radius. Look this figure up in a table of trigonometric functions. The inclusive angle is twice this angle. The use of the number 57.29578 in your method is a sort of quick cheat for finding the angles of long thin triangles. 57.29578 is the cotangent of 1 degree. It is a clever method and apparently yields accurate results if the angles are small. If the rib was as long as the radius the angle would be 57.29 degrees instead of the expected 60 degrees. The other number, .01745 is two times pi divided by 360. This is not a cheat but simply a short hand method. The long version is two times pi times the angle divided by 360. The root of your equation was .01745 times the angle. I don't have time right now but maybe you can find the force necessary to bend a typical uncrowned 2' rib to a 60' radius. Simply apply the force the center of the rib's length. To make it fare you should also scallop the ribs as typically found. I would like to do a little figuring to fine how much force the panel has to exert to form the crown. I think this would be pretty simple and would give us some idea how much of the plastic limit (580 psi) the panel crowned process uses up. I would prefer to call it panel crowned instead of compression crowned. John Hartman
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