000 00497pam a2200133a 44500
082 _aHMSO-R&M-653
_b-
100 _aRose,R.
245 1 _aFLIGHT MEASUREMENTS OF THE DUTCH ROLL CHARACTERISTICS OF A 60 DEGREE DELTA WING AIRCRAFT (FAIREY DELTA 2) AT MACH NUMBERS FROM 0.4 TO 1.5 WITH STABILITY DERIVATIVES EXTRACTED BY VECTOR ANALYSIS
260 _a
_bHer Majesty'S Stationery Office,London
_c1963
300 _a26
500 _aBound With Hmso-R&M-651-60
964 _gCIRC
997 _aTR9026 C
999 _c394828
_d394828