000 | 00549 a2200241 4500 | ||
---|---|---|---|
001 | 313449 | ||
020 | _a | ||
041 | _aeng | ||
080 | _aLNASA TM X 68182 : 1977 | ||
245 | _aEffect of nozzle inlet shape, lip thickness, and exit shape and size on subsonic jet noise | ||
250 | _a | ||
260 | _aWashington, D.C. | ||
260 | _bNational Aeronautics & Space Administration | ||
260 | _c1973 | ||
300 | _a19 p. | ||
300 | _c | ||
856 | _uNASA | ||
490 | _aNASA TM X 68182 : 1977 | ||
700 | _a | ||
650 | _a | ||
650 | _a | ||
942 | _cPP | ||
942 | _2UDC | ||
999 |
_c262179 _d262179 |