000			00419pam a2200133a 44500
082			_aNASA _bTN D-1809
100			_aRe,Richard J
245	1		_aAERODYNAMICS EFFECTS OF MODIFYING WING INBOARD TRAILING-EDGE CAMBER OF A MODEL AT HIGH SUBSONIC SPEEDS.
260			_a _bNasa, Washington, D.C. _c1963
300			_a43
500			_aBound With Nasa Tn D-1801-1808,1810.Lack No-1805
964			_gCIRC
997			_aTR15512 C
999			_c399595 _d399595