| タイトル | Turbulent-flow separation criteria for overexpanded supersonic nozzles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780022611 |
| 著者（英） | Goldberg, T. J.; Morrisette, E. L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1978-08-01 |
| 言語 | eng |
| 内容記述 | A comprehensive compilation of available turbulent flow separation data for overexpanded supersonic nozzles is presented with a discussion of correlation techniques, and prediction methods. Data are grouped by nozzle types: conical, contoured, and two dimensional wedge. Correlation of conical nozzle separation is found to be independent of nozzle divergence half-angle above the 9 deg, whereas the contoured nozzle data follow a different correlation curve. Zero pressure gradient prediction techniques are shown to predict adequately the higher divergence angle conical separation data, and an empirical equation is given for the contoured nozzle data correlation. Flow conditions for which the correlations are invalid are discussed and bounded. A nozzle boundary layer transition criterion is presented which can be used to show that much of the noncorrelating data in the literature are concerned with nonturbulent separation and which explains the previously reported external flow effects on nozzle separation. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 78N30554
NASA-TP-1207
L-11530 |
| 権利 | No Copyright |
