1 / 19

UNSTEADY VISCOUS FLOW

UNSTEADY VISCOUS FLOW. Assume linear, horizontal motion. Viscous effects confined to within some finite area near the boundary → boundary layer. In unsteady viscous flows at low Re the boundary layer thickness δ grows with time; but in periodic flows, it remains constant.

anais
Télécharger la présentation

UNSTEADY VISCOUS FLOW

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. UNSTEADY VISCOUS FLOW Assume linear, horizontal motion Viscous effects confined to within some finite area near the boundary → boundary layer In unsteady viscous flows at low Re the boundary layer thickness δgrows with time; but in periodic flows, it remains constant If the pressure gradient is zero, Navier-Stokes equation (in x) reduces to:

  2. Heat Equation– parabolic partial differential equation - linear Requires one initial condition and two boundary conditions U Impulsively started plate – Stokes first problem y Total of three conditions

  3. Heat Equation– parabolic partial differential equation Can be solved by “Separation of Variables” Suppose we have a solution: Substituting in the diff eq: May also be written as: Moving variables to same side: The two sides have to be equal for any choice of y and t , The minus sign in front of k is for convenience

  4. This equation contains a pair of ordinary differential equations:

  5. Applying B.C., B = 0; C =1; increasing time

  6. Alternative solution to“Separation of Variables” – “Similarity Solution” New independent variable: from: Substituting into heat equation: η is used to transform heat equation:

  7. 2 BC turn into 1 To transform second order into first order: Or in terms of the error function: Integrating to obtain u: With solution: For η > 2 the error function is nearly 1, so that u → 0

  8. For η > 2 the error function is nearly 1, so that u → 0 Then, viscous effects are confined to the region η < 2 This is the boundary layer δ increasing time δgrows as the squared root of time

  9. UNSTEADY VISCOUS FLOW Oscillating Plate – Stokes’ second problem Look for a solution of the form: Ucos(ωt) y Euler’s formula

  10. B.C. in Y Substitution into: Fourier’s transform in the time domain:

  11. Most of the motion is confined to region within: Ucos(ωt) y

  12. UNSTEADY VISCOUS FLOW Oscillating Plate Look for a solution of the form: Ucos(ωt) y W Euler’s formula

  13. B.C. in Y Substitution into: Fourier’s transform in the time domain:

  14. Same solution as for unbounded oscillating plate

More Related