Cross Sectional Area of Jet for given Dynamic Thrust Parallel to Direction of Jet evaluator uses Cross Sectional Area of Jet = (Force by Jet Normal to Plate in X*[g])/(Specific Weight of Liquid*Fluid Jet Velocity^2*(sin(Angle between Jet and Plate))^2) to evaluate the Cross Sectional Area of Jet, Cross Sectional Area of Jet for given Dynamic Thrust Parallel to Direction of Jet is the area of a two-dimensional shape that is obtained when a three-dimensional object - such as a cylinder. Cross Sectional Area of Jet is denoted by AJet symbol.
How to evaluate Cross Sectional Area of Jet for given Dynamic Thrust Parallel to Direction of Jet using this online evaluator? To use this online evaluator for Cross Sectional Area of Jet for given Dynamic Thrust Parallel to Direction of Jet, enter Force by Jet Normal to Plate in X (FX), Specific Weight of Liquid (γf), Fluid Jet Velocity (vjet) & Angle between Jet and Plate (∠D) and hit the calculate button.