CFD capability in the prediction of 3D afterbody flows including cold jet effects were tested in the present work. Comparison of numerical results with available experimental data shows that viscous effects are confined to the region close to the afterbody trailing edge.
Numerical simulation of three-dimensional aircraft afterbodies including jet effects
SIBILLA, STEFANO;
1995-01-01
Abstract
CFD capability in the prediction of 3D afterbody flows including cold jet effects were tested in the present work. Comparison of numerical results with available experimental data shows that viscous effects are confined to the region close to the afterbody trailing edge.File in questo prodotto:
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