| 000 | 01748mm a2200553a 44500 | ||
|---|---|---|---|
| 001 | NM003239 | ||
| 003 | AR-HaUTN | ||
| 007 | ta | ||
| 008 | 73020sc. 1 ||||||||||||||000 | spa|| | ||
| 005 | 20240912185435.0 | ||
| 040 | _aarhautn | ||
| 100 |
_aProuty, Raymond W. _95803 |
||
| 245 |
_aMore helicopter aerodynamics _cRaymond W. Prouty |
||
| 250 | _a[1st?] | ||
| 260 |
_aPeoria _bPJS |
||
| 300 |
_a108 p. _bil. byn, gráficos |
||
| 500 | _aGlosario eíndice alfabético, al final del libro | ||
| 500 | _aNoticia sobre el autor p. 108 | ||
| 505 | _tThe rotor wake | ||
| 505 | _tGround effect in hover | ||
| 505 | _tVortex-ring state | ||
| 505 | _tHover figure of merit and forward flight lift-to drag ratio | ||
| 505 | _tMaximum load factor | ||
| 505 | _tEmergency maneuvering | ||
| 505 | _tIs the rotor a gyro? | ||
| 505 | _tTranslational lift and transverse flow | ||
| 505 | _tFlying in steady winds | ||
| 505 | _tFlight in turbulent air | ||
| 505 | _tSideslip and bank | ||
| 505 | _tInstrument flight | ||
| 505 | _tLow speed power failures | ||
| 505 | _tExternal loads | ||
| 505 | _tAxes system and trim considerations | ||
| 505 | _tThe lead-lag hinge | ||
| 505 | _tDesigning for maneuverability | ||
| 505 | _tDesigning for high speed | ||
| 505 | _tStopping a rotor in flight | ||
| 505 | _tAerodynamic modifications | ||
| 505 | _tComputational fluid dynamics | ||
| 505 | _tFly-by-wire | ||
| 505 | _tSmart control systems | ||
| 505 | _tNew criteria for flying qualities | ||
| 505 | _tLow observables | ||
| 505 | _tLanding gear choices | ||
| 505 | _tCoaxials and synchropters | ||
| 505 | _tWich way should the rotor turn? And where should the pilot sit? | ||
| 505 | _tWindmills | ||
| 942 | _cBK | ||
| 999 |
_c3239 _d3239 |
||