Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) evaluator uses Radial Coordinate = 0.774*Drag Coefficient^(1/3)*(Distance from X-Axis/Diameter)^(2/3) to evaluate the Radial Coordinate, Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) formula is defined as a method to estimate the radial distance from the axis of symmetry to the stagnation point on a blunt-nosed body in hypersonic flight, providing a crucial parameter for velocity and altitude mapping in hypersonic flight paths. Radial Coordinate is denoted by rcylinder symbol.
How to evaluate Blunt-Nosed Radial Coordinate Flat Plate (First Approximation) using this online evaluator? To use this online evaluator for Blunt-Nosed Radial Coordinate Flat Plate (First Approximation), enter Drag Coefficient (CD), Distance from X-Axis (y) & Diameter (d) and hit the calculate button.