000 00490pam a2200145a 44500
082 _aHMSO-R&M-995
_b-
100 _aTurner,K. J., Ross,A. Jean
245 1 _aDYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4
260 _a
_bHer Majesty'S Stationery Office, London
_c1968
300 _a67
500 _aBound With Hmso-R&M-991-99
700 _aEarley,Geraldine
964 _gCIRC
997 _aTR9652 C
999 _c394351
_d394351