Aerodynamic analysis of a canard missile configuration using ANSYS-CFX
Approved for public release, distribution unlimited--Cover. === 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....
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/10707 |