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NASA supersonic tandem canard-controlled missile | Ansys Fluent

$120

Download NASA TCM Ansys-Fluent files.
Download files here
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Version: Ansys Workbench, Fluent v 2020R2 and higher
Contents: CAD, Workbench Mesh+analysis files and result files.
Kindly check description for more details.

NASA supersonic tandem canard-controlled missile is a standard test case used for validating CFD codes for supersonic flow over a missile body. Check the video tutorial for more details.

Analysis mode: Steady State RANS with single periodic domain
Turbulence model : k-w sst
Version : Fluent 2020R2 (In Ansys workbench)

 

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