Fluid Mechanics |
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Page 205
... occurs both a rapid decrease of the velocity and a rapid change of the fluid temperature to a value equal to the temperature of the solid surface . The boundary layer is characterised by the presence of large gradients of both velocity ...
... occurs both a rapid decrease of the velocity and a rapid change of the fluid temperature to a value equal to the temperature of the solid surface . The boundary layer is characterised by the presence of large gradients of both velocity ...
Page 214
... occurs in a fluid between two infinite horizontal planes at different temperatures , that of the lower plane ( T2 ) being greater than that of the upper plane ( T1 ) . If the temperature difference T2 - T1 is small , the fluid remains ...
... occurs in a fluid between two infinite horizontal planes at different temperatures , that of the lower plane ( T2 ) being greater than that of the upper plane ( T1 ) . If the temperature difference T2 - T1 is small , the fluid remains ...
Page 474
... occurs , increasing with the temperature . In many cases this de- pendence is very marked . The speed of the reaction may be so small at ordinary temperatures that the reaction hardly occurs , even though the gas mixture corresponding ...
... occurs , increasing with the temperature . In many cases this de- pendence is very marked . The speed of the reaction may be so small at ordinary temperatures that the reaction hardly occurs , even though the gas mixture corresponding ...
Contents
3 Hydrostatics | 7 |
10 Incompressible fluids | 27 |
11 The drag force in potential flow past a body | 35 |
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Common terms and phrases
adiabatic amplitude angle axis Bernoulli's equation body boundary conditions boundary layer calculation characteristics co-ordinates coefficient combustion constant corresponding cross-section cylinder denote derivative determined detonation wave dimension direction distance drag energy flux entropy equation of continuity equations of motion equilibrium Euler-Tricomi equation Euler's equation expression flow past fluid velocity flux density formula frequency function gas velocity given gives grad gradient heat Hence ideal fluid incompressible increases infinity integral intersection Laplace's equation M₁ mechanical equilibrium moves Navier-Stokes equation obtain oscillations p₁ parameters perturbations pipe plane potential flow pressure PROBLEM propagated quantities radius rarefaction wave result Reynolds number shock wave simple wave small compared solution sound wave sphere spherical streamlines subsonic Substituting superfluid supersonic surface of discontinuity temperature tensor thermal conduction thermodynamic turbulent flow v₁ v₂ vector velocity component velocity of sound viscosity volume weak discontinuity x-axis zero др дх дхк
References to this book
Level Set Methods and Dynamic Implicit Surfaces Stanley Osher,Ronald Fedkiw No preview available - 2002 |