000			00492pam a2200145a 44500
082			_aARC _bR & M 3078
100			_aKirby,D A
245	1		_aLOW-SPEED-TUNNEL MODEL TESTS ON THE FLOW STRUCTURE BEHIND A DELTA-WING AIRCRAFT AND A 4O DEG SWEPT-WING AIRCRAFT AT HIGH INCIDENCES
260			_a _bHer Majesty'S Stationery Office, London _c1958
300			_a15
500			_aBound With Arc R & M 3070-3077,3079-3080,Lack No. 3075
700			_aSpence,A
964			_gCIRC
997			_aTR14423 C
999			_c398758 _d398758