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

V.P. Zamuraev; A.P. Kalinina

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

机译：在超声管流动上的热和气体动力动作中形成跨音质区域

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摘要

The control simultaneous action of a jet and near-wall energy sources on the shockwave structure of a supersonic 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.

机译：射流和近壁能源对轴对称和平面管道中的超声波流动冲击波结构的控制同步动作是为了产生跨音区域的目的。获得具有扩展跨型静脉区域的制度。

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来源
《Thermophysics and Aeromechanics》 |2018年第1期|共4页
作者
V.P. Zamuraev; A.P. Kalinina;
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作者单位

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

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

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原文格式 PDF
正文语种 eng
中图分类热学与物质分子运动论;
关键词
supersonic flow; duct; near-wall energy sources; jet; Euler and Navier-Stokes equations;

机译：超音速流动;管道;近壁的能源;喷射;欧拉和Navier-Stokes方程;

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专利

1. Transonic region formation at the thermal and gas-dynamic action on a supersonic duct flow [J] . V.P. Zamuraev, A.P. Kalinina Thermophysics and Aeromechanics . 2018,第1期

机译：在超声管流动上的热和气体动力动作中形成跨音质区域
2. Definition of the Existence Region of the Solution of the Problem of an Arbitrary Gas-dynamic Discontinuity Breakdown at Interaction of Flat Supersonic Jets with Formation of Two Outgoing Compression Shocks [J] . Pavel Viktorovich Bulat, Mikhail Pavlovich Bulat Research journal of applied science, engineering and technology . 2015,第1期

机译：平面超声速射流相互作用并形成两个输出压缩激波时任意气体动力不连续性破坏问题解的存在区域的定义
3. Definition of the Existence Region of the Solution of the Problem of an Arbitrary Gas-dynamic Discontinuity Breakdown at Interaction of Flat Supersonic Jets with Formation of Two Outgoing Compression Shocks [J] . Pavel Viktorovich Bulat, Mikhail Pavlovich Bulat Research journal of applied science, engineering and technology . 2015,第1期

机译：平面超声速射流相互作用并形成两个输出压缩激波时任意气体动力不连续性破坏问题解的存在区域的定义
4. Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply [C] . V. P. Zamuraev, A. P. Kalinina International Conference on the Methods of Aerophysical Research . 2018

机译：通过喷射和近壁输电控制在超音速流动中形成跨音区域形成
5. A THEORETICAL AND EXPERIMENTAL INVESTIGATION OF TRANSONIC FLOW IN THE THROAT REGION OF ANNULAR AXISYMMETRIC, SUPERSONIC NOZZLES [D] . DUTTON, JONATHAN CRAIG -1

机译：环形轴对称，超音速喷管的喉部跨音速流动的理论和实验研究
6. Free boundary problems in shock reflection/diffraction and related transonic flow problems [O] . Gui-Qiang Chen, Mikhail Feldman -1

机译：冲击反射/衍射中的自由边界问题以及相关的跨音速流动问题
7. Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply [O] . V. P. Zamuraev, A. P. Kalinina 2018

机译：通过喷射和近壁输电控制在超音速流动中形成跨音区域形成

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

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