Abstract
A single computation is compared with experimental results for Test case 1: hypersonic boundary layer on a cone. A computation is compared with experiment for the base flow over an axisymetric downward step behind the cone inducing a fully detached and turbulent hypersonic flow. At the conference more computations were presented so occasional comments about them are also made.
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© 1991 Springer-Verlag Berlin Heidelberg
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Pironneau, O. (1991). A Synthesis of Results for Test Cases 1 and 2: Hypersonic Boundary Layer and Base Flow. In: Désidéri, JA., Glowinski, R., Périaux, J. (eds) Hypersonic Flows for Reentry Problems. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-76527-8_12
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DOI: https://doi.org/10.1007/978-3-642-76527-8_12
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-76529-2
Online ISBN: 978-3-642-76527-8
eBook Packages: Springer Book Archive