000 | 00608nam a2200157 4500 | ||
---|---|---|---|
003 | OSt | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
245 |
_aPrediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [ NASA TM X-3134] _cCarl J. Daniele, Ronald J.Blaha and Kurt Seldner |
||
260 |
_aWashington D.C. _bNational Aeronaticsand Space Administration _c1975 |
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300 | _a34p | ||
440 | _aNational Aeronaticsand Space Administration (NASA) | ||
650 | _aDigital computer | ||
700 | _aBlaha,Ronald. J. and Seldner, Kurt | ||
942 | _cBK | ||
999 |
_c564461 _d564461 |