xphiliac007
Aerospace
- Oct 1, 2007
- 5
Hello all,
I had a particular question concerning the fatigue crack growth data listed in Appendix F of API 579-1/ASME FFS-1 (2007 ed).
I am analyzing a pressure vessel constructed out of SA-302 Gr. B (mod.) material with a yield strength (Sy) of 100 ksi. Typically we use the Paris Law to determine our number number of cycles to failure using API 579 as a source for fatigue crack growth data. The constants C, n, and Eyr is determined based on Sy of the material, composition (grain structure), temperature, and outside environment that the material is exposed to. Since Sy is 100 ksi, I have to refer to Section F.5.3.3 to get my constants, but how do I determine if SA-302 Gr. B is a martensitic steel or ferritic-pearlite steel? Can that be determined simply by chemical composition, or if the material has been heat treated, etc.? Thanks in advance.
I had a particular question concerning the fatigue crack growth data listed in Appendix F of API 579-1/ASME FFS-1 (2007 ed).
I am analyzing a pressure vessel constructed out of SA-302 Gr. B (mod.) material with a yield strength (Sy) of 100 ksi. Typically we use the Paris Law to determine our number number of cycles to failure using API 579 as a source for fatigue crack growth data. The constants C, n, and Eyr is determined based on Sy of the material, composition (grain structure), temperature, and outside environment that the material is exposed to. Since Sy is 100 ksi, I have to refer to Section F.5.3.3 to get my constants, but how do I determine if SA-302 Gr. B is a martensitic steel or ferritic-pearlite steel? Can that be determined simply by chemical composition, or if the material has been heat treated, etc.? Thanks in advance.