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Factor de carga

De Wikipedia, la enciclopedia libre

En aeronáutica el factor de carga es la razón existente entre la fuerza de sustentación que se produce en una aeronave en vuelo y el peso de esta.[1]​ El aumento del factor de carga es directamente proporcional a la tensión que la estructura de la aeronave tendrá que soportar en ciertas condiciones límite.

Referencias

  1. Hurt, H.H. (1960). Aerodynamics for Naval Aviators. A National Flightshop Reprint. Florida.

Véase también

Esta página se editó por última vez el 4 sep 2019 a las 14:35.
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