A B C D E F G H I J K L M N O P Q R S T U V W X Y



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.
Subárea
Aircraft Structure
Related Term
blade
blade angle
blade root
stall
Spanish
pérdida de sustentación de las palas