Oct 12, 2017 #1 fede_vx Mechanical Oct 12, 2017 6 We had to double check the calculation made by a chinese engineering team and we figured out almost everything except the formula at row 34. Can anybody help? https://i.imgur.com/aJpB75K.jpg
We had to double check the calculation made by a chinese engineering team and we figured out almost everything except the formula at row 34. Can anybody help? https://i.imgur.com/aJpB75K.jpg
Oct 12, 2017 #2 ewh Aerospace Mar 28, 2003 6,147 Please do not duplicate postings. "Know the rules well, so you can break them effectively." -Dalai Lama XIV Upvote 0 Downvote
Please do not duplicate postings. "Know the rules well, so you can break them effectively." -Dalai Lama XIV
Oct 12, 2017 Thread starter #3 fede_vx Mechanical Oct 12, 2017 6 Sorry... Didn't know exactly where to post it Upvote 0 Downvote
Oct 12, 2017 #4 rb1957 Aerospace Apr 15, 2005 16,057 if line 33 is the stress at bolt 2 (section A2-A2), it looks like the load applied it the load applied at bolt 1 ? is line 35 the allowable stress ? another day in paradise, or is paradise one day closer ? Upvote 0 Downvote
if line 33 is the stress at bolt 2 (section A2-A2), it looks like the load applied it the load applied at bolt 1 ? is line 35 the allowable stress ? another day in paradise, or is paradise one day closer ?
Oct 13, 2017 Thread starter #5 fede_vx Mechanical Oct 12, 2017 6 Found it! Roark table 13.5. Upvote 0 Downvote
Oct 13, 2017 #6 rb1957 Aerospace Apr 15, 2005 16,057 should the full load be applied at all locations ? another day in paradise, or is paradise one day closer ? Upvote 0 Downvote
should the full load be applied at all locations ? another day in paradise, or is paradise one day closer ?
