| 000 | 00638 a2200241 4500 | ||
|---|---|---|---|
| 001 | 284308 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 1293 : 1978 | ||
| 245 | _aPerformance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region | ||
| 250 | _a | ||
| 260 | _aWashington,D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1978 | ||
| 300 | _a82 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TP 1293 : 1978 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aTurbomachinery, Transonic compressors, Inlet radial distortion | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c243570 _d243570 |
||