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Aerodynamic analysis of a canard missile configuration using ANSYS-CFX

This study used the Computational Fluid Dynamics code, ANSYS-CFX to predict the static aerodynamic characteristics of a canard-wing missile configuration with a hemispherical nose, triangular wedge canards and fixed trapezoidal wings. The study was conducted for Mach numbers of 0.2, 0.8 and 1.2.
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Full Core Calculation for FRM II with Serpent 2 and Ansys CFX

International Conference on Physics of Reactors (PHYSOR 2024)
Kaltrina Shehu, Christian Reiter
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