Jun 2, 2015 #1 addagalla Aerospace Joined Oct 24, 2012 Messages 3 Location IN we are modelling some bolted joints using CBUSH elements in FEM. can anybody help what is the difference in using huth method and using AG/L to calculate shear stiffness. Thanks in Advance.
we are modelling some bolted joints using CBUSH elements in FEM. can anybody help what is the difference in using huth method and using AG/L to calculate shear stiffness. Thanks in Advance.
Jun 2, 2015 #2 rb1957 Aerospace Joined Apr 15, 2005 Messages 16,133 Location CA um, huth's equation is not AG/L ... (that'd be the difference) another day in paradise, or is paradise one day closer ? Upvote 0 Downvote
um, huth's equation is not AG/L ... (that'd be the difference) another day in paradise, or is paradise one day closer ?
Jun 3, 2015 #3 SWComposites Aerospace Joined Nov 6, 2000 Messages 3,717 Location US Most of the joint flexibility is not fastener shear deformation. Have you read Huth's paper? Upvote 0 Downvote
Jun 3, 2015 Thread starter #4 addagalla Aerospace Joined Oct 24, 2012 Messages 3 Location IN I have not read Huth's paper. But what I am doing wrong if i Use AG/L as CBUSH stiffness. Upvote 0 Downvote
Jun 3, 2015 #5 RPstress Aerospace Joined Jun 4, 2003 Messages 846 Location GB You will be overestimating the stiffness and this should predict more load transferred on the first fastener. http://files.engineering.com/getfile.aspx?folder=c9483ab2-674a-4137-b36b-04704f132608&file=Huth,_Influence_of_Fastener_Flexibility_(stiffness)__on_the_Prediction_of_Load_Transfer_and_Fatigue_Life_for_Multiple-Row_Joints.pdf Upvote 0 Downvote
You will be overestimating the stiffness and this should predict more load transferred on the first fastener.
Jun 3, 2015 #6 SWComposites Aerospace Joined Nov 6, 2000 Messages 3,717 Location US Agreed. Way too stiff by only considering fastener shear deformation. Best approach - fab a two row joint specimen, test it, measure displacement. Then correlate your FEM approach to the test. Upvote 0 Downvote
Agreed. Way too stiff by only considering fastener shear deformation. Best approach - fab a two row joint specimen, test it, measure displacement. Then correlate your FEM approach to the test.