This invention provides a full-
physics field simulation test device and method for shipborne aircraft fuel fires based on wind-
wave coupling effects, relating to
fire safety. The device includes: a shipborne aircraft
simulation component comprising an aircraft support,
fuel tank, attitude adjustment mechanism, and at least one ammunition simulator; a ship
simulation component comprising a fuel pan and a swing mechanism connected to the fuel pan; a
sea breeze environment
simulation component comprising a water mist spraying mechanism and a fan; and a
data acquisition system for collecting data on the
wind field,
flame, and surface temperature and
radiant heat flux of the ammunition simulator under wind-
wave coupling conditions, thereby quantifying the degree of
thermal stimulation of the ammunition under different operating conditions. The beneficial effects of this invention are: it enables the simulation of dynamic ammunition thermal
exposure of shipborne aircraft under ocean wind-
wave coupling conditions, filling the research gap in existing technologies that can only simulate static ammunition thermal
exposure, and enabling a systematic study of the
impact of ammunition attitude changes on the uniformity of thermal
exposure.