000 00548pam a2200145a 44500
082 _aARC
_bR&M 3355
100 _aThompson,J S
245 1 _aOSCILLATORY-DERIVATIVE MEASUREMENTS ON STINGMOUNTED WING-TUNNEL MODELS
_bMETHOD OF TEST AND RESILTS FOR PITCH AND YAW ON A CAMBERED OGEE WING AT MACH NUMBERS UP TO 2.6
260 _a
_bHer Majesty'S Stationery Office, London
_c1964
300 _a52
500 _aBound Wiyh:Arc R&M 3341-3354,3356-3360.Lack No.Arc R&M 3343,45,49,50,53,59
700 _aFail,R A
964 _gCIRC
997 _aTR11186 C
999 _c395338
_d395338