Email this article Control of the structure of flow around a rhomboid wing in supersonic flow
- Authors: Zubin M.A.1, Maksimov F.A.1, Ostapenko N.A.1
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Affiliations:
- Lomonosov Moscow State University
- Issue: Vol 485, No 3 (2019)
- Pages: 290-294
- Section: Mechanics
- URL: https://journals.eco-vector.com/0869-5652/article/view/12846
- DOI: https://doi.org/10.31857/S0869-56524853290-294
- ID: 12846
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Abstract
Certain results of the numerical investigation of the possibility of controlling the structure of flow near a V-shaped wing with an opening angle greater than p under an asymmetric flow around by a supersonic stream under the regimes with shock waves attached to the leading edges or with a centered rarefaction wave on the lee console are presented.
About the authors
M. A. Zubin
Lomonosov Moscow State University
Author for correspondence.
Email: zubinma@mail.ru
Russian Federation, 1, Leninskie gory, Moscow, 119991
F. A. Maksimov
Lomonosov Moscow State University
Email: zubinma@mail.ru
Russian Federation, 1, Leninskie gory, Moscow, 119991
N. A. Ostapenko
Lomonosov Moscow State University
Email: zubinma@mail.ru
Russian Federation, 1, Leninskie gory, Moscow, 119991
References
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- Зубин М. А., Остапенко Н. А. // Изв. АН СССР. МЖГ. 1983. № 6. С. 43-51.
- Зубин М. А., Максимов Ф. А., Остапенко Н. А. // Изв. РАН. МЖГ. 2014. № 6. С. 118-134.
- Зубин М. А., Максимов Ф. А., Остапенко Н. А. // ДАН. 2014. Т. 454. № 3. С. 282-288.
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