000			00566pam a2200145a 44500
008			160408b1970 xxu||||| |||| 00| 0 eng d
082			_aARC _bC.P. 1108
100			_aLawford,J A
245	1		_aLOW SPEED WIND-TUNNEL TESTS ON AN UNSWEPT WING-FUSELAGE MODEL OF ASPECT RATIO 9.8, WITH TANGENTIAL BLOWING OVER TRAILING-EDGE FLAPS AND AILERONS, INCLUDING THE EFFECT OF SLIPSTREAM
260			_a _bHer Majesty'S Stationery Office, London _c1970
300			_a21
500			_aBound With Arc C.P.1100-1107,1109-1110 Lack No.1104
964			_gCIRC
997			_aA13862 C
999			_c273693 _d273693