000 00562 a2200241 4500
001 275381
020 _a
041 _aeng
080 _aLNASA CR 3925 : 1985
245 _aUnstady flow in a supersonic cascade with two in-passage shocks
250 _a
260 _aWashington, D.C.
260 _bNational Aeronautics and Space Adminstration
260 _c1985
300 _a89 p.
300 _c
856 _u
490 _aNASA CR 3925 : 1985
700 _a
650 _a
650 _aFlutter, Compressor, Supersonic flow, Shock waves
942 _cPP
942 _2UDC
999 _c232820
_d232820