000 00413pam a2200133a 44500
082 _a-
_b-
100 _aWatson,J.
245 1 _aCALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM
260 _a
_bHer Majesty'S Stationery Office,London
_c1958
300 _a34
500 _aBound With Hmso-R&M-3050-69
964 _gCIRC
997 _aTR892 C
999 _c394826
_d394826