@RPstress : Sorry I did not point out to ultimate shear allowable load Fsu...
@rb1957: Actually, the most (may be all) of the shear load is transferred based on the "vertical" part of the rivet shank (also for shear area: pi*d^4/4, d is the diameter of the rivet shank). The reason whey only one...
Dears,
I know that this topic has been appraoched several times through many named threads but there is still some confusion (to me) on the subject...I would like to know if anyone is used to following bearing allowable stress: Sbr=Fsu/(d*(t-0.5*CSK)
where t is the sheet thickness, d is the...
SWComposites said:
"For thin skin sandwich panels, repair depths can usually be the full thickness of the facesheet, and peridoic inspections are usually not required."
Do you mean that only the thin thickness can be riveted using a doubler? do you have any available document or reference that...
Hello,
I am looking for a link to download Tom Swift paper "Repairs to Damage Tolerant Aircraft".
May anyone help me with that.
Thank you much in advance.
regards,