000 00431pam a2200133a 44500
082 _aC.P.
_b1140
100 _aHuntley,E
245 1 _aWIND TUNNEL TESTED AT TRANSONIC AND SUPERSONIC SPEEDS TO INVESTIGATE THE LONGITUDINAL STABILITY OF A MODEL OF THE AVRO 720 AIRCRAFT.
260 _a
_bHer Majesty'S Stationery Office, London
_c1971
300 _a48
500 _aBound With C.P.1131-39
964 _gCIRC
997 _aTR10587 C
999 _c396175
_d396175