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Abstract
A turbulent flow field is created in a vehicle’s head during high-speed flight, and this flow field causes the airborne optical system’s receiving target images to be displaced, blurred, and jittered. In this study, we examine the impact of a 0°–15° angle of attack on the aero-optical imaging deviation. With the use of modeling and meshing software, we created a model of a conventional blunt-headed vehicle. Computational fluid dynamics calculations were performed using finite element analysis software; the ray equations were solved iteratively by the Runge–Kutta method. Finally, the imaging deviation data were obtained by using reverse ray tracing and tracing stop criteria. The findings demonstrate that, as the angle of attack increases from 0° to 15°, the thickness of the nonuniform flow field above the vehicle flow field cross-section axis gradually increases. As the density of the nonuniform flow field through which light propagates increases, so does the corresponding refractive index and the aero-optical imaging deviation.
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