In the elastic case, column-buckling (or critical) stress can be predicted using the Euler stringers that can experience inter-rivet buckling. Further details can be. This paper deals with the modelling of hybrid composites and is focused on a detailed simulation of the inter-rivet buckling behaviour in a stiffened fuselage shell. Inter-rivet buckling of stiffener flanges fastener spacing, s. • flange under compression buckles with a half-wave length equal to the fastener spacing. • fasteners.
|Published (Last):||26 February 2011|
|PDF File Size:||4.10 Mb|
|ePub File Size:||13.29 Mb|
|Price:||Free* [*Free Regsitration Required]|
Thank you for helping keep Eng-Tips Forums free from inappropriate posts. The Eng-Tips staff will check rviet out and take appropriate action. Click Here to join Eng-Tips and talk with other members! Join your peers on the Internet’s largest technical engineering professional community.
Bjckling easy to join and it’s free. Register now while it’s still free! Close this window and log in. Are you an Engineering professional? By joining you are opting in to receive e-mail.
An investigation of inter-rivet buckling of aircraft panels in compression
Promoting, selling, recruiting, coursework and thesis posting is forbidden. Can somebody shed some light on the difference between Wrinkling vs Inter-rivet buckling. Is one more critical than the other on a riveted skin panel? I would define wrinkling as a form of buckling of a panel, regardless of its means of being fastened. The wrinkles can extend beyond any fastener group and may not be associated with any fasteners at all.
Wrinkling can be produced by shear, not necessarily compression.
Inter-rivet buckling, on the other hand, involves an area of material that has deflected significantly between the fasteners, regardless of the overall shape or size of the panel. IR buckling is usually associated with compression in the joint with the fasteners.
Do you ibter a copy of Bruhn? Which is more critical? That depends on a bunch of variables; just do both checks. Wrinkling isn’t always a failure mode, it can be the onset of the panel going into semi shear tension. Inter-rivet buckling is an instability that occurs between two adjacent rivets in a stiffener, the strap of skin between two rivets bukcling as if it were a wide column supported by a rivet on each end. Wrinkling is a skin buckle that continues through a stiffener attach flange possibly to the adjacent panel, the behavior is mostly driven by rivet spacing and the distance between the rivets and an upstanding stiffener web.
Which is more critical depends on the panel. The handbook of structural stability is a good reference too pdf: Both of those references are basically summarized in Bruhn. Something to consider when talking about inter rivet buckling, is the observed item truly inter rivet buckling, or is it something caused by displaced material from bucking the rivets too hard.
I’ve seen this intwr of time where the skin layout was done correctly, but when assembled, the skin puckered up between the rivets after the rivets were driven too hard and actually displaced material under the head of the rivet.
Sometimes this condition gets set up when a “cleco”,a common fastener slips or looses it’s grip on the two different work pieces. Its not common but when noticed it was assumed that it was stress induced,after much concern and study,it was reazlized integ it was shop practices that were to blame.
There was a problem providing the content you requested
The spring in the cleco becomes worn and losses its ability to hold tightly the two pieces being joined,and slippage occurs,rather than stopping at that point most riveters continue the operation,all looks pretty normal,but intdr a little while the excess material that had bunched up shows up as a ripple ot wrinkle. It was latter realized that worn out springs in the cleco’s were the cause.
Some of these temporary holding or clamping devices have been arounr since before ww-2,ans are still in use. After my first post I did some digging into brugn and also with a research paper. My findings are bucklin This do no deform the attached flange. Thus wrinkling failure is a combination of skin and flange failure and could occur due to high shear stress as well.
At both these instances, these loads will induce tension loads on attached fasteners and fasteners need to be checked in tension Thank you for your replies.
rkvet My only problem with it is the way it’s organized,it may seem logical for some readers,but not for me. I inteer one time thought about re doing it in my logic pattern to make it easier to use or more systematic,but it may well and probably is my logic pattern that is not logical,so I left well enough alone,probably be a legal nightmare in itself.
Your conclusions are concise and to the point,and I can see no error it their logic,good rules to go by. Just to complicate the picture.
Just about ever GA aircraft out there has waviness induced by the natural-out-of-flat condition of the raw sheet aluminum stock.
Often adjacent open bays may have opposite tendencies: The technical term for ‘oil-canning’ is [gasp!!! The problem with oil-canning is [generally speaking], fatigue cracking at periphery fastener holes rivwt to the large nuckling of oil canning cycles per flight [which are riget usually heard].
Even though flight loading can mitigate the problem for awhile, still experiences various stress states in non-static-flight conditions; and eventually the structure still has-to return to it’s normal static state when tied-up on the flight line.
Red Flag This Post Please let us know here why this post is inappropriate. Reasons such as off-topic, duplicates, flames, illegal, vulgar, or students posting their homework. Digital Transformation may be defined in a number of different ways by analysts or enterprise software vendors. Defense manufacturing is all about project manufacturing and project accounting. Students Click Here Join Us!
Posting Guidelines Promoting, selling, recruiting, coursework and thesis posting is forbidden. Wrinkling vs Inter-rivet buckling Wrinkling vs Inter-rivet buckling Can somebody shed some light intfr the difference between Wrinkling vs Inter-rivet buckling.
Wrinkling vs Inter-rivet buckling I would define wrinkling as a form of buckling of a panel, regardless of its means of being fastened. Wrinkling vs Inter-rivet buckling Which is more critical? Wrinkling vs Inter-rivet buckling Wrinkling isn’t always a failure mode, it can be the onset of the panel going into semi shear tension. Wrinkling vs Inter-rivet buckling Inter-rivet buckling is an instability that occurs between two adjacent rivets in a stiffener, the strap of skin between two rivets buckles as if it were a wide column supported by a rivet on each end.
Riveh vs Inter-rivet buckling Something to consider when talking about inter rivet buckling, is the observed item truly inter rivet buckling, or is it something caused by displaced material from bucking the rivets too hard. Wrinkling vs Inter-rivet buckling Sometimes this condition gets set up when a “cleco”,a common fastener slips or looses it’s grip on the two different work pieces. Wrinkling vs Inter-rivet buckling After my first post I did some digging into brugn and also with a research paper.
Resources Digital Transformation may be defined in a number of different ways by analysts or enterprise software vendors.
Download Now Defense manufacturing is all about project manufacturing and project accounting. Download Now White Paper: