NDLI: Usm3d predictions of supersonic nozzle flow

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Usm3d predictions of supersonic nozzle flow

Content Provider	NASA Technical Reports Server (NTRS)
Author	Nayani, Sudheer N. Campbell, Richard L. Carter, Melissa B. Elmiligui, Alaa A.
Copyright Year	2014
Description	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 data sets. The study showed that with the use of volume sourcing, USM3D was able to capture and model a jet plume's shear layer and internal shock structure.
File Size	4231336
Page Count	18
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20140011460
Archival Resource Key	ark:/13960/t8rc22659
Language	English
Publisher Date	2014-06-16
Access Restriction	Open
Subject Keyword	Fluid Mechanics And Thermodynamics Aerodynamics Grid Refinement Mathematics Computational Fluid Dynamics Shock Wave Interaction Flow Characteristics Sonic Booms Plumes Shear Layers Nozzle Flow Supersonic Nozzles Tetrahedrons Supersonic Jet Flow Mathematical Models Computational Grids Grid Generation Mathematics Signatures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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