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straight-and-level flight
Definição1
A condition when a rotorcraft is in straight-and-level, unaccelerated flight, and all forces are in balance.
Fonte1
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.
Definição2
Flight with a constant heading and at a constant altitude.
Fonte2
FEDERAL AVIATION ADMINISTRATION. Helicopter flying handbook (FAA-H8083-21A). Washington, DC: FAA, 2012.
Fonte3
BRASIL. Comando da Aeronáutica. Departamento de Controle do Espaço Aéreo. AIC-N 06/14: aproximações visuais e decolagens com separação visual para o Aeroporto Internacional de Guarulhos (SBGR). Rio de Janeiro, 2014. Disponível em: http://servicos.decea.gov.br/arquivos/publicacoes/107bacfa-8871-445b-9e5c8df2a6f3b21e.pdf?CFID=017be123-6cec-47b3-adca-48992b66bf10&CFTOKEN=0. Acesso em: 15 maio 2014.
Contexto
In steady-state flight, the helicopter has a load factor of one, which means the main rotor system is supporting the actual total weight of the helicopter. If you increase the bank angle to 60°, while still maintaining a constant altitude, the load factor increases to two.
When in straight-and-level flight, any increase in the collective, while holding airspeed constant, causes the helicopter to climb. A decrease in the collective, while holding airspeed constant, causes the helicopter to descend. A change in the collective requires a coordinated change of the throttle to maintain a constant r.p.m.
Subárea1
Piloting
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