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Wind-Us Unstructured Flow Solutions for a Transonic Diffuser - Stanley R. Mohler,Nasa Technical Reports Server (Ntrs)

English
2013-06-01
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The Wind-US Computational Fluid Dynamics flow solver computed flow solutions for a transonic diffusing duct. The calculations used an unstructured (hexahedral) grid. The Spalart-Allmaras turbulence model was used. Static pressures along the upper and lower wall agreed well with experiment, as did velocity profiles. The effect of the smoothing input parameters on convergence and solution accuracy was investi ... Full description

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Description

The Wind-US Computational Fluid Dynamics flow solver computed flow solutions for a transonic diffusing duct. The calculations used an unstructured (hexahedral) grid. The Spalart-Allmaras turbulence model was used. Static pressures along the upper and lower wall agreed well with experiment, as did velocity profiles. The effect of the smoothing input parameters on convergence and solution accuracy was investigated. The meaning and proper use of these parameters are discussed for the benefit of Wind-US users. Finally, the unstructured solver is compared to the structured solver in terms of run times and solution accuracy.

More Information

Author Stanley R. Mohler, Nasa Technical Reports Server (Ntrs)
Publisher BiblioLife
Release year 2013
Cover type Softcover
EAN 9781289143633
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€20.40 €25.50