Nose Radius of Cylinder-Wedge evaluator uses Radius = Local Shock-Detachment Distance/(0.386*exp(4.67/(Mach Number^2))) to evaluate the Radius, The Nose Radius of Cylinder-Wedge formula is defined as a measure of the radius of a cylinder-wedge shape in hypersonic inviscid flow, which is critical in understanding the aerodynamic characteristics of vehicles and projectiles at high speeds, particularly in the context of re-entry vehicles and spacecraft. Radius is denoted by r symbol.
How to evaluate Nose Radius of Cylinder-Wedge using this online evaluator? To use this online evaluator for Nose Radius of Cylinder-Wedge, enter Local Shock-Detachment Distance (𝛿) & Mach Number (M) and hit the calculate button.