swMATH ID: 3508
Software Authors: Chakrabartty, S.K.; Dhanalakshmi, K.; Mathur, J.S.
Description: Computation of three-dimensional transonic viscous flow using the JUMBO3D code The authors report computational results obtained with a vertex-based finite-volume method for solving the Reynolds-averaged Navier-Stokes-equations for three-dimensional flows. Standard solution elements are used for the construction of the solution. The flow fields computed include the flow past a \(65^circ\) swept cropped delta wing at transonic speeds, the flow past the ONERA M6 wing, and the flow past a multi-body launch vehicle configuration. Compared are the surface pressure distributions which show fair to good agreement with experimental data.
Homepage: http://www.springerlink.com/content/u50t0815r08476x6/fulltext.pdf
Keywords: vertex-based finite-volume method; Reynolds-averaged Navier-Stokes-equations; swept cropped delta wing; ONERA M6 wing; multi-body launch vehicle configuration
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Cited in: 2 Publications

Cited in 1 Serial

2 Acta Mechanica

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