Fluid Mechanics for Engineering Technology

airplane altitude angle of attack applied aspect ratio Assume Bernoulli equation C₁ Chapter Clark Y airfoil Coanda effect constant control jet density depth determine diameter dimensional dimensional analysis drag coefficient energy enthalpy equal Flanged fluid flowing Fluid Mechanics fluid statics fluidic fluidic devices friction factor ft/sec ft² function gage gal/min h₁ h₂ horizontal Hydraulic ideal gas ILLUSTRATIVE PROBLEM inlet isentropic John Wiley laminar flow lb/ft³ level flight lift liquid loss Mach number manometer mass maximum mercury nozzle obtain P₁ pipe plane plate power jet pressure drop psia radius relative Reproduced with permission Reynolds number Screwed shear stress shown in Figure Solution specific weight steady flow Steel stream surface temperature tube turbulent V₁ V₂ valve velocity viscosity volume weir Wiley & Sons wing York Z₁ zero Δρ