| 000 | 00607 a2200241 4500 | ||
|---|---|---|---|
| 001 | 284442 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 1345 : 1978 | ||
| 245 | _aAnalysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1978 | ||
| 300 | _a57 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TP 1345 : 1978 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aActuator disk theory, Flutter, Supersonic speeds, Compressors | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c243711 _d243711 |
||