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Numerical strip-yield calculation of ctod
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Forman, Royce Beek, Joachim |
| Copyright Year | 2007 |
| Description | Many existing methods to calculate CTOD can be costly and complicated, or apply only to particular configurations. A new numerical method for calculating CTOD was investigated. NASGRO's Boundary Element module NASBEM was adapted to calculate displacements at any point on the crack. Demonstrated for a number of crack configurations: a) finite and infinite domains; b) center and edge cracks; and c) complex cases with several cracks and holes. Great accuracy at minimal computational cost. |
| File Size | 438658 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20070017318 |
| Archival Resource Key | ark:/13960/t8tb6358h |
| Language | English |
| Publisher Date | 2007-04-16 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Domains Cracks Costs Edge Cracks Boundaries Displacement Holes Mechanics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |