| タイトル | Aerodynamic stability analysis of NASA J85-13/planar pressure pulse generator installation |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810006489 |
| 著者（英） | Chung, K.; Hosny, W. M.; Steenken, W. G. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1980-11-01 |
| 言語 | eng |
| 内容記述 | A digital computer simulation model for the J85-13/Planar Pressure Pulse Generator (P3 G) test installation was developed by modifying an existing General Electric compression system model. This modification included the incorporation of a novel method for describing the unsteady blade lift force. This approach significantly enhanced the capability of the model to handle unsteady flows. In addition, the frequency response characteristics of the J85-13/P3G test installation were analyzed in support of selecting instrumentation locations to avoid standing wave nodes within the test apparatus and thus, low signal levels. The feasibility of employing explicit analytical expression for surge prediction was also studied. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N15004
NASA-CR-165141
R80AEG429 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170432 |
