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BASIC PRINCIPLES OF FLUID MECHANICS
Stress at a Point
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airfoil axis Bernoulli's equation body boundary layer Chap chapter component compressible computations consider constant continuity equation control surface control volume coordinates curve cylinder developed diagram differential equation dimensional dimensionless groups discussion drag duct employ energy exit expression fluid element force formulations free surface free-stream friction given gradient head loss heat transfer Hence incompressible flow inertial infinitesimal integral irrotational isentropic laminar flow law of thermodynamics Mach lines Mach number Mach waves mass momentum equation normal Note nozzle particle perfect gas pipe plane position pound mass pressure Prob problem psia quantities ratio 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 unit vector velocity field velocity potential velocity profile viscosity law wave zero