<< blade span axis | blade stall | bleed >>
Back to: "B"
blade stall
- Definição1
- The condition of the rotor blade when it is operating at an angle of attack greater than the maximum angle of lift. This occurs at high forward speed to the retreating blade and all blades during "settling with power".
- Fonte1
- SCHAFER, Joe. Helicopter maintenance. Englewood: Jeppesen Sanderson, Inc., c2007. viii, 343 p.
- Definição2
- The condition of the rotor blade when it is operating at an angle of attack greater than the maximum angle of lift.
- Fonte2
- FEDERAL AVIATION ADMINISTRATION. Rotorcraft flying handbook (FAA-H-8083-21). Washington, DC: FAA, 2000. Disponível em: http://www.faa.gov/library/manuals/aircraft/media/faa-h-8083-21.pdf. Acesso em: 10 fev. 2012.
- Fonte3
- FEDERAL AVIATION ADMINISTRATION. Rotorcraft flying handbook (FAA-H-8083-21). Washington, DC: FAA, 2000. Disponível em:
- Contexto
- You can avoid retreating blade stall by not exceeding the never-exceed speed.
- Subárea1
- Engine
- Related Term
- stall
- Português
- estol de pá