dcascap
Aerospace
- Feb 6, 2024
- 24
Hi,
I'm using the NAS1204 bolt in a design and I encounter the following:
The tensile stress allowable vs the tension force allowable on this spec significantly differs (for around a factor of 1.3) if we compared it by converting the stress allowable to equivalent tension allowable, as F=sigma*A with A the tensile stress area.
I think it can be due to the countersunk head, which will lead to a different type of failure (stresses in countersunk are quite difficult to assess), and which it reflects in the tension allowable, assuming that the tension allowables are tested values.
Do you know if my reasoning is okay? or do you have a better explanation? Thanks in advance!
Attached a screenshot of the spec .
I'm using the NAS1204 bolt in a design and I encounter the following:
The tensile stress allowable vs the tension force allowable on this spec significantly differs (for around a factor of 1.3) if we compared it by converting the stress allowable to equivalent tension allowable, as F=sigma*A with A the tensile stress area.
I think it can be due to the countersunk head, which will lead to a different type of failure (stresses in countersunk are quite difficult to assess), and which it reflects in the tension allowable, assuming that the tension allowables are tested values.
Do you know if my reasoning is okay? or do you have a better explanation? Thanks in advance!
Attached a screenshot of the spec .