MECHANICS OF FLUIDS1962 |
Contents
Stress at a Point | 18 |
Fluid Statics | 34 |
Foundations of Flow Analysis | 73 |
Copyright | |
41 other sections not shown
Other editions - View all
Common terms and phrases
airfoil axis Bernoulli's equation body boundary layer Chap chapter component computations consider constant continuity equation control surface control volume coordinates curve developed diagram differential equation dimensional dimensionless groups drag duct employ energy exit expression fluid element force formulations free surface friction given gradient head loss heat transfer Hence incompressible flow inertial infinitesimal integral irrotational isentropic laminar flow law of thermodynamics Mach number Mach waves mass momentum equation normal nozzle particle Patm perfect gas pipe plane position pound mass pressure Prob problem psia quantities region relation replace result Reynolds number shear stress shock shown in Fig stagnation steady flow stream function streamline subsonic flow supersonic flow temperature tion torque turbine turbulent flow two-dimensional V₁ V₂ vector velocity field velocity potential velocity profile viscosity law wave zero მე მყ