000 00348 a2200133 4500
001 90385
082 _aPR 890
090 _c42705
_d42705
100 _aAbdul Hayee
245 _aDesign of a turbo jet engine axial flow compressor
_nG-21
260 _aKarachi
_bNED University
_c1985
300 _a118 p.
_bhand written
500 _aBE Project Reports
942 _aCAE NUST
_kPR 890
999 _c325458
_d325458