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 |