Control of the structure of flow around a rhomboid wing in supersonic flow

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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

  1. Максимов Ф. А., Остапенко Н. А. // ДАН. 2016. Т. 469. № 6. С. 680-685.
  2. Зубин М. А., Максимов Ф. А., Остапенко Н. А. // ДАН. 2017. Т. 477. № 4. С. 410-414.
  3. Зубин М. А., Остапенко Н. А. // Изв. АН СССР. МЖГ. 1983. № 6. С. 43-51.
  4. Зубин М. А., Максимов Ф. А., Остапенко Н. А. // Изв. РАН. МЖГ. 2014. № 6. С. 118-134.
  5. Зубин М. А., Максимов Ф. А., Остапенко Н. А. // ДАН. 2014. Т. 454. № 3. С. 282-288.

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