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Computational composite mechanics for aerospace propulsion structures
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chamis, Christos C. |
| Copyright Year | 1987 |
| Description | Specialty methods are presented for the computational simulation of specific composite behavior. These methods encompass all aspects of composite mechanics, impact, progressive fracture and component specific simulation. Some of these methods are structured to computationally simulate, in parallel, the composite behavior and history from the initial frabrication through several missions and even to fracture. Select methods and typical results obtained from such simulations are described in detail in order to demonstrate the effectiveness of computationally simulating: (1) complex composite structural behavior in general, and (2) specific aerospace propulsion structural components in particular. |
| File Size | 823084 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870009181 |
| Archival Resource Key | ark:/13960/t4xh4gz09 |
| Language | English |
| Publisher Date | 1987-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Finite Element Method Turbine Blades Fiber Composites Metal Matrix Composites Fracture Strength Composite Structures Engine Parts Impact Damage Aerospace Engineering Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
