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...
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,