JUMBO3D 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 Related Software: Cited in: 2 Publications Cited by 3 Authors 2 Chakrabartty, Sunil Kumar 2 Dhanalakshmi, K. S. 2 Mathur, J. S. Cited in 1 Serial 2 Acta Mechanica Cited in 1 Field 2 Fluid mechanics (76-XX) Citations by Year