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High performance fibers for structurally reliable metal and ceramic composites. [advanced gas turbine engine materials]
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dicarlo, J. A. |
| Copyright Year | 1984 |
| Description | Very few of the commercially available high performance fibers with low densities, high Young's moduli, and high tensile strengths possess all the necessary property requirements for providing either metal matrix composites (MMC) or ceramic matrix composites (CMC) with high structural reliability. These requirements are discussed in general and examples are presented of how these property guidelines are influencing fiber evaluation and improvement studies at NASA aimed at developing structurally reliable MMC and CMC for advanced gas turbine engines. |
| File Size | 801685 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850003787 |
| Archival Resource Key | ark:/13960/t1hj1c48t |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Boron Fibers Fiber Strength Aluminum Boron Composites Reinforcing Fibers Gas Turbine Engines Impact Resistance Silicon Carbides Metal Matrix Composites Ceramics Microstructure Matrix Materials Crack Propagation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
