Hypersonic Aerodynamics and Heat Transfer
ISBN Imprimir: 978-1-56700-309-3
ISBN On-line: 978-1-56700-287-4
DOI: 10.1615/978-1-56700-309-3.0
Chapter 16: Numerical Method of Solving Viscous Shock Layer Equations in a Wide Range of Reynolds Numbers
DOI: 10.1615/978-1-56700-309-3.300
Table of contents
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