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Structural analysis of cylindrical thrust chambers, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Armstrong, W. H. |
| Copyright Year | 1981 |
| Description | Analytical results are presented which predict cumulative plastic deformation characteristic of damage observed in coolant channel walls of regeneratively cooled rocket thrust chambers. The damage consists of bulging and plastic flow which leads to thinout and rupture of the channel wall under the combined effects of high pressures, high temperatures and temperature gradients experienced during cyclic firings of actual test chambers. Analytical predictions correlate with test results. |
| File Size | 1508170 |
| Page Count | 68 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810018657 |
| Archival Resource Key | ark:/13960/t23c0vt7j |
| Language | English |
| Publisher Date | 1981-03-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Finite Element Method Performance Prediction Rocket Engine Cases Coolants Thrust Chambers Plastic Deformation Combustion Chambers Elastic Deformation Walls Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
