Loading...
Please wait, while we are loading the content...
Similar Documents
Advanced turbine technology applications project (attap) (Document No: 19950009329)
Technical Report
Industry tests of nasa ceramic thermal barrier coating. [for gas turbine engine applications
Article
Reliability of ceramics for heat engine applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1980 |
| Description | The advantages and disadvantages associated with the use of monolithic ceramics in heat engines are discussed. The principle gaps in the state of understanding of ceramic material, failure origins, nondestructive tests as well as life prediction are included. |
| File Size | 9105730 |
| Page Count | 156 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800020840 |
| Archival Resource Key | ark:/13960/t9q28qq9z |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Nondestructive Tests Life Durability Quality Control Gas Turbine Engines Failure Modes Reliability Analysis Ceramics Hot Corrosion 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 |