000 00596 a2200241 4500
001 357659
020 _a
041 _aeng
080 _aDARC R&M 3485 : 1965
245 _aFlight measurement of the elevator and aileron hinge-moment derivatives of the fairey delta 2 aircraft upto a Mach number of 1.6 and comparisons with wind-tunnel results
250 _a
260 _aLondon
260 _bHer Majesty's Stationary Office
260 _c1965
300 _a16 p.
300 _c
856 _u
490 _aARC R&M 3485 : 1965
700 _a
650 _a
650 _a
942 _cPP
942 _2UDC
999 _c229201
_d229201