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Boundary-Layer Theory

By: Schlichting, Hermann.
Contributor(s): Kestin, J. (Translated By).
Material type: materialTypeLabelBookPublisher: New York Mc Graw Hill Book Company 1968Edition: 6th.Description: 747.Subject(s): ElectronicsDDC classification: 629.13237
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Books Books BSDU Knowledge Resource Center, Jaipur
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629.13237 SCH (Browse shelf) Available DB0141

Contents :
Part A : Fundamental laws of motion for a viscous fluid
Chapter 1 : Outline of fluid motion with friction
Chapter 2 : Outline of boundary-layer thery
Chapter 3 : Derivation of equations of motion of a compressible viscous fluid (Navier -Stocks equations )
Chapter 4 : General properties of the Navier-Stokes equations
Chapter 5 : Exact solutions of the Navier -Stokes equation
Chapter 6 : Very slow motion

Part B : Laminar boundary layers

Chapter 7 Boundary layer equation for two-dimensional flow ; boundary on a place
Chapter 8 : General properties of the boundary - layer eqations
Chapter 9 : Exact solution of the steady -state boundary -layer equations in two dimensional motion
Chapter 10 : Approximate methods for the solution of the two-dimensional ,steady boundary -layer equations
Chapter 11 : Axially symmetrical and three -dimensional boundary layers
Chapter 12 : Thermal boundary layers in laminar flow
Chapter 13 Laminar boundary in natural flow
Chapter 14 :Boundary -layer control in laminar flow
Chapter 15 : Non-Steady boundary layers

Part C : Transition

Chapter 16 : Origin of turbulence I
Chapter 17 : Origin of turbulence II

Part D Turbulent boundary layers

Chapter 18 :Fundamentals of turbulent flow
Chapter 19 :Theoretical assumption for the calculations of turbulent flows
Chapter 20 :Turbulent flow through pipes
Chapter 21 :Turbulent boundary layers at zero pressure gradient ;flat plate ;rotation disks ; roughness
Chapter 22 : The incompressible turbulent bounadary layer with pressure gradient
Chapter 23 : Turbulent boundary layers in compressible flow
Chapter 24 : Free tubulent flow ; jets and wakes
Chapter 25 Determination of profile drag

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