000 00575nam a2200145 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
300 _a34p
440 _aNational Aeronaticsand Space Administration (NASA)
700 _aBlaha,Ronald. J. and Seldner, Kurt
942 _cBK
999 _c564460
_d564460