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