000			00458pam a2200133a 44500
082			_aARC _bC.P. 1005
100			_aPowell,B J
245	1		_aTHE CALCULATION OF THE PRESSURE DISTRIBUTION ON A THICK CAMBERED AEROFOIL AT SUBSONIC SPEEDS INCLUDING THE EFFECTS OF THE BOUNDARY LAYER.
260			_a _bHer Majesty'S Stationery Office, London _c1967
300			_a30
500			_aBound With Arc C.P.1000-1004, 1006-1009
964			_gCIRC
997			_aTR10830 C
999			_c395732 _d395732