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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.
openaire   +1 more source

Modelling of condensing steam flows in Laval nozzles with ANSYS CFX

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2018
exaly  

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