Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow


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Abstract

The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a superso-nic flow in the axisymmetric and planar ducts is studied for the purpose of creating a transonic region. The regimes with an extended transonic region are obtained.

About the authors

V. P. Zamuraev

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Author for correspondence.
Email: Zamuraev@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk

A. P. Kalinina

Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

Email: Zamuraev@itam.nsc.ru
Russian Federation, Novosibirsk; Novosibirsk


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