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 Z


<< K | KE | KG >>

Back to: "K"

KE
Usado para
kinetic energy
Definição1
Energy of motion.
Fonte1
CROCKER, David. Dictionary of aviation. 2nd ed. London: A&C, 2005.
Fonte2
WORLD METEOROLOGICAL ORGANIZATION. Guide to meteorological observing and information distribution systems for aviation weather services. Geneva, Switzerland, 2014. (WMO, n.731). ISBN 978-92-63-10731-2.
Fonte3
INTERNATIONAL CIVIL AVIATION ORGANIZATION. Aerodrome design manual. Part VI: frangibillity. Montreal, 2006 (Doc. 9157 AN/901).
Fonte4
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, 2017. Disponível em: . Acesso em: 28 junho. 2022.
Nota adicional1
The kinetic energy required for acceleration of the fragments, or the total structure in the case of a one-piece design, is calculated using the known mass and the representative aircraft velocity.
Nota adicional2
(1) The brake kinetic energy absorption requirements must be based on a conservative rational analysis of the sequence of events expected during landing at the design landing weight. (2) Instead of a rational analysis, the kinetic energy absorption requirements for each mainwheel brake assembly may be derived from the following formula: KE=0.0443 WV2/N where: KE=Kinetic energy per wheel (ft.-lb.); W=Design landing weight (lb.); V=Airplane speed in knots. V must be not less than VS √, the poweroff stalling speed of the airplane at sea level, at the design landing weight, and in the landing configuration; and N=Number of main wheels with brakes.
Contexto
In the thermodynamic scale of temperature, measurements are expressed as differences from absolute zero (0 K), the temperature at which the molecules of any substance possess no kinetic energy.
Português
energia cinética