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


<< power-on stall | power-to-weight ratio | power unit >>

Back to: "P"

power-to-weight ratio
Fonte1
AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL (Brasil). Regulamento Brasileiro de Aviação Civil: RBAC n. 23: requisitos de aeronavegabilidade: aviões categoria normal, utilidade, acrobática e transporte regional. Brasília, 2013. Disponível em: . Acesso em: 06 maio 2016.
Contexto
75 percent of maximum continuous power. However, if the power-to-weight ratio at 75 percent of maximum continuous power results in extreme nose-up attitudes, the test may be carried out with the power required for level flight in the landing configuration at maximum landing weight and a speed of 1.4 VSO, except that the power may not be less than 50 percent of maximum continuous power.
Spanish
relación potencia/peso