| タイトル | Coordinates for a High Performance 4:1 Pressure Ratio Centrifugal Compressor |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970024917 |
| 著者（英） | McKain, Ted F.; Holbrook, Greg J. |
| 著者所属（英） | Detroit Diesel Allison |
| 発行日 | 1997-07-01 |
| 言語 | eng |
| 内容記述 | The objective of this program was to define the aerodynamic design and manufacturing coordinates for an advanced 4:1 pressure ratio, single stage centrifugal compressor at a 10 lbm/sec flow size. The approach taken was to perform an exact scale of an existing DDA compressor originally designed at a flow size of 3.655 lbm/sec. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | 97N24621
NASA-CR-204134
NAS 1.26:204134
E-10833 |
| 権利 | No Copyright |
