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ISSN Online: 2377-424X

ISBN Print: 978-1-56700-474-8

ISBN Online: 978-1-56700-473-1

International Heat Transfer Conference 16
August, 10-15, 2018, Beijing, China

COMPUTER SIMULATION OF THERMOPHYSICAL PROCESSES IN SHOCK WAVE GENERATORS

Get access (open in a dialog) DOI: 10.1615/IHTC16.nee.020916
pages 7745-7752

Аннотация

The thermal processes in the hypersonic aerodynamic shock tube are considered. Feature of the proposed approach is numerical calculation of processes deriving the quasi-one-dimensional equations of gas dynamics, using dynamically adaptive grids. Aerodynamic studies in the single diaphragm shock tube are conducted. Shock tube flows and waves are investigated. The pressure distribution, Mach number distribution and the temperature distribution are presented. The experimental and calculated time dependences of the pressure are compared.