000			00490pam a2200145a 44500
082			_aARC _bR&M 3004
100			_aHenshall,B D
245	1		_aTHE INTERACTION BETWEEN SHOCK WAVES AND BOUNDARY LAYERS AT THE TRAILING EDGE OF A DOUBLE-WEDGE AEROFOIL AT SUPERSONIC SPEED.
260			_a _bHer Majesty'S Stationery Office, London _c1957
300			_a10
500			_aBound With Arc R&M 3000-3002, 3005-19 Lack No. 3003,13,15.
700			_aCash,R F
964			_gCIRC
997			_aTR11039 C
999			_c395479 _d395479