An assessment of unstructured grid finite volume schemes for cold gas hypersonic flow calculations
A comparison of five different spatial discretization schemes is performed considering a typical high speed flow application. Flowfields are simulated using the 2-D Euler equations, discretized in a cell-centered finite volume procedure on unstructured triangular meshes. The algorithms studied inclu...
Main Authors: | , |
---|---|
Format: | Article |
Language: | English |
Published: |
Instituto de Aeronáutica e Espaço (IAE)
2009-06-01
|
Series: | Journal of Aerospace Technology and Management |
Subjects: | |
Online Access: | http://www.jatm.com.br/papers/vol1_n2/JATMv1n2_p135-152_An_assessment_of_unstructured_grid_finite_volume_schemes_for_cold_gas_hypersonic_flow_calculations.pdf |