000 | 00733 a2200289 4500 | ||
---|---|---|---|
001 | 73706 | ||
020 | _a92-835-0573-59 | ||
041 | _aeng | ||
080 | _a621.438:533.6.01 Pro | ||
245 | _aPropulsion and energetics panel working group 18 on test cases for computation of internal flows in aero engine components / edited by L. Fottner | ||
250 | _a | ||
260 | _a | ||
260 | _bNeuilly sur Seine : AGARD, 1990 | ||
260 | _c1990 | ||
300 | _aix,379 p. | ||
300 | _c29 cm | ||
490 | _a | ||
100 | _a | ||
700 | _a | ||
650 | _a | ||
650 | _aAxial flow compressors | ||
650 | _aTurbines-Aerodynamics | ||
650 | _aTurbomachines-Aerodynamics | ||
650 | _aGas turbines-Aerodynamics | ||
942 | _cBK | ||
942 | _2UDC | ||
999 |
_c76387 _d76387 |