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Pre-host high temperature crack propagation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Orange, T. W. |
| Copyright Year | 1982 |
| Description | The highlights of NASA contract CR-167896, Fracture Mechanics Criteria for Turbine Engine Hot Section Components, are presented. The five technical tasks of the program are reviewed. Results of several tasks are presented. |
| File Size | 233174 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850002648 |
| Archival Resource Key | ark:/13960/t5fb9wh6f |
| Language | English |
| Publisher Date | 1982-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Finite Element Method Fracture Mechanics Gas Turbine Engines Louvers Aircraft Engines High Temperature Crack Initiation Crack Propagation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |