<p>In this article, we prove that the threshold of instability of the classical Couette flow in <InlineEquation ID="IEq1"> <InlineMediaObject> <ImageObject Color="BlackWhite" FileRef="220_2025_5401_Article_IEq1.gif" Format="GIF" Height="14" Rendition="HTML" Resolution="72" Type="Linedraw" Width="24" /> </InlineMediaObject> <EquationSource Format="TEX">\(H^s\)</EquationSource> <EquationSource Format="MATHML"><math> <msup> <mi>H</mi> <mi>s</mi> </msup> </math></EquationSource> </InlineEquation> for large <i>s</i> is <InlineEquation ID="IEq2"> <InlineMediaObject> <ImageObject Color="BlackWhite" FileRef="220_2025_5401_Article_IEq2.gif" Format="GIF" Height="18" Rendition="HTML" Resolution="72" Type="Linedraw" Width="29" /> </InlineMediaObject> <EquationSource Format="TEX">\(\nu ^{1/2}\)</EquationSource> <EquationSource Format="MATHML"><math> <msup> <mi>ν</mi> <mrow> <mn>1</mn> <mo stretchy="false">/</mo> <mn>2</mn> </mrow> </msup> </math></EquationSource> </InlineEquation>. The instability is completely driven by the boundary. The dynamic of the flow creates a Prandtl type boundary layer of width <InlineEquation ID="IEq3"> <InlineMediaObject> <ImageObject Color="BlackWhite" FileRef="220_2025_5401_Article_IEq2.gif" Format="GIF" Height="18" Rendition="HTML" Resolution="72" Type="Linedraw" Width="29" /> </InlineMediaObject> <EquationSource Format="TEX">\(\nu ^{1/2}\)</EquationSource> <EquationSource Format="MATHML"><math> <msup> <mi>ν</mi> <mrow> <mn>1</mn> <mo stretchy="false">/</mo> <mn>2</mn> </mrow> </msup> </math></EquationSource> </InlineEquation> which is itself linearly unstable. This leads to a secondary instability which in turn creates a sub-layer.</p>

错误:搜索内容不能为空,请输入英文关键词
错误:关键词超出字数限制,请精简
高级检索

Boundary Driven Instabilities of Couette Flows

  • Dongfen Bian,
  • Emmanuel Grenier,
  • Nader Masmoudi,
  • Weiren Zhao

摘要

In this article, we prove that the threshold of instability of the classical Couette flow in \(H^s\) H s for large s is \(\nu ^{1/2}\) ν 1 / 2 . The instability is completely driven by the boundary. The dynamic of the flow creates a Prandtl type boundary layer of width \(\nu ^{1/2}\) ν 1 / 2 which is itself linearly unstable. This leads to a secondary instability which in turn creates a sub-layer.