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DLF
- Usado para
- 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.)
- Subárea1
- Operations
- Português
- fator de carga de projeto