| タイトル | Development of a simplified procedure for thrust chamber life prediction |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820013379 |
| 著者（英） | Badlani, M.; Porowski, J. S.; Peterson, D.; Kasrale, B.; Odonnell, W. J. |
| 著者所属（英） | O'Donnell and Associates, Inc. |
| 発行日 | 1981-10-01 |
| 言語 | eng |
| 内容記述 | An analytical design procedure for predicting thrust chamber life considering cyclically induced thinning and bulging of the hot gas wall is developed. The hot gas wall, composed of ligaments connecting adjacent cooling channel ribs and separating the coolant flow from the combustion gas, is subjected to pressure loading and severe thermal cycling. Thermal transients during start up and shut down cause plastic straining through the ligaments. The primary bending stress superimposed on the alternate in-plane cyclic straining causes incremental bulging of the ligaments during each firing cycle. This basic mechanism of plastic ratcheting is analyzed and a method developed for determining ligament deformation and strain. The method uses a yield surface for combined bending and membrane loading to determine the incremental permanent deflection and pregressive thinning near the center of the ligaments which cause the geometry of the ligaments to change as the incremental strains accumulate. Fatigue and tensile instability are affected by these local geometry changes. Both are analyzed and a failure criterion developed. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 82N21253
NAS 1.26:165585
ODAI-1403-12-81
NASA-CR-165585 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166510 |
