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Selection the first hovering shock wave in the field of gas jet flow
E. V. Afanasiev, S. V. Bobyshev, I. L. Dobroserdov Baltic State Technical University
Abstract:
It is given a description of the mathematical model that permits us to build a first hovering shock wave of Laval's nozzle at the expiration of a supersonic jet. This model was worked out within the framework of the structure-element method that orientats us towards creating high-speed software of engineering calculated methods.
Received: 20.09.2000 Revised: 03.02.2003
Citation:
E. V. Afanasiev, S. V. Bobyshev, I. L. Dobroserdov, “Selection the first hovering shock wave in the field of gas jet flow”, Matem. Mod., 15:11 (2003), 13–29
Linking options:
https://www.mathnet.ru/eng/mm372 https://www.mathnet.ru/eng/mm/v15/i11/p13
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Statistics & downloads: |
Abstract page: | 410 | Full-text PDF : | 271 | References: | 50 | First page: | 1 |
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