## Fluid Mechanics for Engineering TechnologyPrentice-Hall, 1970 - 366 pages |

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airfoil airplane angle of attack applied Assume body channel Chapter coefficient consider constant depth derived determine devices diameter difference direction drag drop effect element energy Engineering equal equation flow fluid flowing Fluid Mechanics fluidic force friction ft/sec function gage given head heat horizontal ILLUSTRATIVE PROBLEM increase known laminar lb/ft³ length lift liquid loss manometer mass maximum measured mercury MICHIGAN necessary noted nozzle obtain operated pipe plane plate possible pounds pressure psia quantity radius reference relative Reynolds number Screwed shown in Figure shows side Solution solve specific weight square steady Steel stream surface surface tension Table temperature tube turbulent unit V₁ valve velocity viscosity volume wall weir wing York zero