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Fluid DynamicsPart 3 Boundary Layers$
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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

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Introduction

Introduction

Chapter:
(p.1) Introduction
Source:
Fluid Dynamics
Author(s):

Anatoly I. Ruban

Publisher:
Oxford University Press
DOI:10.1093/oso/9780199681754.003.0001

This book investigates high-Reynolds number flows, and analyses flows that can be described in the framework of Prandtl’s 1904 classical boundary-layer theory, including Blasius’s boundary layer on a flat plate, Falkner–Skan solutions for the boundary layer on a wedge surface, and other applications of Prandtl’s theory. It then discusses separated flows, and considers the so-called ‘self-induced separation’ in supersonic flow, and which led to the ‘triple-deck model’. It also presents Sychev’s 1972 theory of the boundary-layer separation in an incompressible fluid flow past a circular cylinder. It discusses the triple-deck flow near the trailing edge of a flat plate, and then considers the incipience of the separation at corner points of the body surface in subsonic and supersonic flows. It covers the Marginal Separation theory—a special version of the triple-deck theory—and describes the formation and bursting of short separation bubbles at the leading edge of a thin aerofoil.

Keywords:   boundary-layer theory, viscous-inviscid interaction, triple-deck theory, separated flows, high-Reynolds number flows, Prandtl, Falkner–Skan

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