- PII
- 10.31857/S0032823524060045-1
- DOI
- 10.31857/S0032823524060045
- Publication type
- Article
- Status
- Published
- Authors
- Volume/ Edition
- Volume 88 / Issue number 6
- Pages
- 874-886
- Abstract
- Planar supersonic flows of inviscid gas, obeyed the Abel – Noble (AN) equation of state, are considered. Formulas connecting flow parameters of considered gas before and after shock wave are obtained. Solution of Prandtl–Meyer problem for flow of AN gas in centered rarefaction fan is constructed. Critical values of velocity vectors turn angle in oblique shock wave and rarefaction fan are found. Comparisons with corresponding solution for perfect gas are given.
- Keywords
- сверхзвуковые течения газ Абеля–Нобля ударная волна течение Прандтля–Майера
- Date of publication
- 01.06.2024
- Year of publication
- 2024
- Number of purchasers
- 0
- Views
- 34
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