| タイトル | IPAC-Inlet Performance Analysis Code |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970025646 |
| 著者（英） | Barnhart, Paul J. |
| 著者所属（英） | NYMA, Inc. |
| 発行日 | 1997-07-01 |
| 言語 | eng |
| 内容記述 | A series of analyses have been developed which permit the calculation of the performance of common inlet designs. The methods presented are useful for determining the inlet weight flows, total pressure recovery, and aerodynamic drag coefficients for given inlet geometric designs. Limited geometric input data is required to use this inlet performance prediction methodology. The analyses presented here may also be used to perform inlet preliminary design studies. The calculated inlet performance parameters may be used in subsequent engine cycle analyses or installed engine performance calculations for existing uninstalled engine data. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | 97N25142
NASA-CR-204130
NAS 1.26:204130
E-10800 |
| 権利 | No Copyright |
|
