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USM3D predictions of Supersonic Nozzle Flow
2014
32nd AIAA Applied Aerodynamics Conference
unpublished
This study focused on the NASA Tetrahedral Unstructured Software System CFD code (USM3D) capability to predict supersonic plume flow. Previous studies, published in 2004 and 2009, investigated USM3D's results versus historical experimental data. This current study continued that comparison however focusing on the use of the volume souring to capture the shear layers and internal shock structure of the plume. This study was conducted using two benchmark axisymmetric supersonic jet experimental
doi:10.2514/6.2014-2270
fatcat:dxhfcq2wn5blhdv5y7wyxvpeyq