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AbstractAbstract
[en] Finite-difference methods are improved to calculate two-dimensional transonic and supersonic flows in nozzles taking into account the kinetics of nonequilibrium phase transitions. A comparison with experimental data testifies to the improved accuracy of the methods under consideration
Primary Subject
Source
Translated from Inzhenerno-Fizicheskii Zhurnal; 63: No. 2, 199-204(Aug 1992).
Record Type
Journal Article
Literature Type
Numerical Data; Translation
Journal
Journal of Engineering Physics and Thermophysics; ISSN 1062-0125;
; CODEN JEPTER; v. 63(2); p. 808-812

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