000			00437pam a2200145a 44500
082			_aNACA _bTM-1420
100			_aCorcos,G M
245	1		_aON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE
260			_a _bNational Advisory Committee For Aeronautics, Washington,D.C. _c1956
300			_a43
500			_aBound With Naca Tm-1421-1429.
700			_aLiepmann,H W
964			_gCIRC
997			_a17288 C
999			_c448817 _d448817