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Back to: "D"design load factor
- Definição1
- Maximum repeated vertical acceleration which an aircraft structure is designed to withstand without accretion of damage. Typical values for a jet transport are +2·5/-1g (with flaps extended reduced to +2), and for a fighter +12/-6.
- Fonte1
- GUNSTON, Bill. The cambridge aerospace dictionary. Cambridge: Cambridge University, 2004. vii, 740 p. (Cambridge aerospace series.)
- Fonte2
- ASSOCIAÇÃO BRASILEIRA DE NORMAS TÉCNICAS. NBR 13537: carga aérea e equipamento de apoio no solo para aeronave – vocabulário. Rio de Janeiro, 2006.
- Nota adicional1
- Acronym in English: DLF.
- Subárea1
- Operations
- Related Term
- load factor
- Português
- fator de carga de projeto