000 01246mm a2200397a 44500
001 NM000215
003 AR-HaUTN
005 20240917163957.0
007 ta
008 97120s1994 ||||||||||||||000 | spa||
020 _a0340587024
040 _aAR-HaUTN
_cAR-HaUTN
100 _aNewman, Simon
_93
245 _aThe foundations of helicopter flight
_cSimon Newman
250 _a1th ed.
260 _aLondon
_bEdward Arnold
300 _aviii, 303 p.
500 _aIndice analítico y abreviaturas, en páginas preliminares
500 _aIndice alfabético, al final del libro
504 _aReferencias bibliográficas p. 291298
505 _tRotorcraft configurations
505 _tThe rotor in hover
505 _tThe rotor in axial flightclimb and descent
505 _tThe rotor in forward flight
505 _tDynamics of the rotor
505 _tAutorotative performance
505 _tBlade dynamics
505 _tHelicopter trims
505 _tVibration and its transmission
505 _tTail rotors
505 _tGround resonance
505 _tRotor speed governing
505 _tMethods of calculating helicopter power, fuel consumption and mission performance
505 _tThe windmill
942 _cBK
_2udc
999 _c215
_d215