NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
T0TEM - T0 Test Evaluation Module Development and VerificationTransition temperature testing of ferritic steels evaluates the ductile to brittle transition temperature, where the behavior of the steel changes from controlled ductile tearing to uncontrollable brittle fracture. This testing is governed by ASTM (American Society of Testing and Materials) E1921 standard. The calculations and plots required by this standard are iterative in nature and require significant effort to produce by standard hand calculations. In addition to analysis of a complete data set, intermediate analysis during testing is beneficial to determine optimal test temperatures. Given the exhaustive nature of calculating the transition temperature, being able to quickly update target temperatures is a significant benefit to not only the quality of tests, but the number of required tests as well. T0 Test Evaluation Module (T0TEM) v1.5 is a software application created under the Layered Pressure Vessel (LPV) certification effort. To reduce the analysis time of transition temperature test data sets producedfor this effort, T0TEM was created to calculate the E1921 Master Curve along with all required data and validity checks. By creating this program, hundreds of hours of analysis time were saved. In addition, the creation of a standard program provided a significant improvement in the consistency with which results were reported. T0TEM also calculates the results and plots required for the E1921 inhomogeneity annex to determine whether a material behaves in a homogenous manner. This program was created by Levi Shelton and Cameron Bosley at NASA, with input and review from the E1921 committee. The results generated by T0TEM were compared to the validation data sets provided by ASTM with good concurrence. ASTM committee members have reviewed and applied T0TEM to other data sets with satisfactory results. T0TEM was originally released to the NASA Software Repository and publicly via SourceForge in May of 2020. Version 1.5 was released in April of 2021 with minor functionality updates and additional statistical analysis methods.
Document ID
20210020028
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Levi Shelton
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Cameron Bosley
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
August 5, 2021
Publication Date
August 1, 2021
Publication Information
Subject Category
Computer Programming And Software
Physics (General)
Funding Number(s)
PROJECT: 817091.30.50.62.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
No Preview Available