Jump to ContentJump to Main Navigation
Fluid DynamicsPart 3 Boundary Layers$
Users without a subscription are not able to see the full content.

Anatoly I. Ruban

Print publication date: 2017

Print ISBN-13: 9780199681754

Published to Oxford Scholarship Online: January 2018

DOI: 10.1093/oso/9780199681754.001.0001

Show Summary Details
Page of

PRINTED FROM OXFORD SCHOLARSHIP ONLINE (www.oxfordscholarship.com). (c) Copyright Oxford University Press, 2020. All Rights Reserved. An individual user may print out a PDF of a single chapter of a monograph in OSO for personal use. date: 28 January 2020

Boundary-Layer Separation

Boundary-Layer Separation

Chapter:
(p.143) 2 Boundary-Layer Separation
Source:
Fluid Dynamics
Author(s):

Anatoly I. Ruban

Publisher:
Oxford University Press
DOI:10.1093/oso/9780199681754.003.0003

Chapter 2 discusses the experimental observations of the boundary-layer separation in subsonic and supersonic flows that lead to a formulation of the concept of viscous-inviscid interaction. It then turns to the so-called ‘self-induced separation’ of the boundary layer in supersonic flows. This theory is formulated based on the asymptotic analysis of the Navier–Stokes equations at large values of the Reynolds number. As a part of the flow analysis, this chapter also introduces the ‘triple-deck model’. It then shows how this model may be used to describe the classical problem of the boundary-layer separation in an incompressible fluid flow past a circular cylinder.

Keywords:   viscous-inviscid interaction, self-induced separation, triple-deck model, Navier–Stokes equations, supersonic flows, Reynolds number

Oxford Scholarship Online requires a subscription or purchase to access the full text of books within the service. Public users can however freely search the site and view the abstracts and keywords for each book and chapter.

Please, subscribe or login to access full text content.

If you think you should have access to this title, please contact your librarian.

To troubleshoot, please check our FAQs , and if you can't find the answer there, please contact us .