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Nothing on cross-referencing but both rivets are made from L86 (2117-T4) material. The SP71 being a solid 100-degree countersink and the SP80 being a solid Protruding head. They are intended to replace rivets made from L37 (2014 T4) removing the need to store in the fridge before installation.

Don't know if you have seen this thread on eng-tips forum 'Metal and Mettallurgy Egineering', dated July 2003, I found it by typing 'ESDU' and 'BS970' on Google. He's basically asking the same question as you and a number of reference sources are given in responce. If AISI 4340 is nearly...

JMW Thanks for the suggestion, but I'm using Word 2000 and 'settings' doesn't appear on the edit tab. I aasume this option is given on 2002 onwards. Cheers.

Just read that there is a restriction maximum limit for the amount of information an Excel object can display. They thought it was about 70 rows, which ties up exactly with where my table was being truncated. However, I think this is based on a standard row height of 12.75, so by reducing the...

Am I right in assuming that the net goes over the top of the cargo and attaches to the floor inb'd/Outb'd and fore and aft? Is the cargo placed in standard containers before being covered by the the net?

Thanks for the replies. The problem I have with using the simple cut and paste (Ctrl C and V) is that it simply reproduces the Excel cells in Word table format. When the table is to big to fit in side the page borders you have to scale it down by adjusting the individual row and column...

I've had this problem before and I don't think I solved it then. I'm trying to copy a table from Excel to a Word document using paste special. If I choose to paste either as a 'picture' or as an 'object' the final few rows don't appear. If I insert an additional row into the middle of the table...

Thanks for the replies, If I understood you correctly, I’ve just tried reducing the E value in the material card to practically zero and I get the same results as with the panels not being there, altering the G value made no difference at all. Basically, it seems to have just one mode of...

I’m trying to de-idealise results from a very large existing aircraft FE Model. The model contains a number of TRIA3 elements in the fuselage side skins and I can’t quite workout how these elements are working. If you de-idealise them using the grid point forces as you would a QUAD4 it would...