About the features of hypersonic flow past a yawed plate

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Abstract


The flow around the yawed plate in the regime of strong interaction is considered in the case when the pressure at its trailing edge is not constant, but changes along the transverse coordinate. It is shown that in the case of large transverse gradients of the induced pressure, the type of expansions of flow functions in the vicinity of the leading edge changes significantly and the third term of the expansions should be taken into account.


About the authors

G. N. Dudin

The Central AeroHydrodynamic Institute named after Prof. N.E. Zhukovsky

Author for correspondence.
Email: gndudin@yandex.ru

Russian Federation, 1, Zhukovsky Street, TsAGI Zhukovsky, Moscow Region, 140180

V. Ya. Neyland

The Central AeroHydrodynamic Institute named after Prof. N.E. Zhukovsky

Email: gndudin@yandex.ru

Russian Federation, 1, Zhukovsky Street, TsAGI Zhukovsky, Moscow Region, 140180

Corresponding Member of the Russian Academy of Sciences

References

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