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Fatigue crack growth model random2 user manual, appendix 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Boyce, Lola Lovelace, Thomas B. |
| Copyright Year | 1989 |
| Description | The FORTRAN program RANDOM2 is documented. RANDOM2 is based on fracture mechanics using a probabilistic fatigue crack growth model. It predicts the random lifetime of an engine component to reach a given crack size. Included in this user manual are details regarding the theoretical background of RANDOM2, input data, instructions and a sample problem illustrating the use of RANDOM2. Appendix A gives information on the physical quantities, their symbols, FORTRAN names, and both SI and U.S. Customary units. Appendix B includes photocopies of the actual computer printout corresponding to the sample problem. Appendices C and D detail the IMSL, Ver. 10(1), subroutines and functions called by RANDOM2 and a SAS/GRAPH(2) program that can be used to plot both the probability density function (p.d.f.) and the cumulative distribution function (c.d.f.). |
| File Size | 1313343 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890014519 |
| Archival Resource Key | ark:/13960/t6g20wh4w |
| Language | English |
| Publisher Date | 1989-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Metal Fatigue Service Life Fatigue Life Component Reliability Engine Parts User Manuals Computer Programs Probability Density Functions Fortran Crack Propagation Subroutines Stress Intensity Factors Failure Analysis Cracking Fracturing Applications Programs Computers Prediction Analysis Techniques Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |