Stress in Flat Blade evaluator uses Stress in Blade = (Force)*(0.75*Radius of Impeller Blade-Radius of Hub)/(Blade Thickness*Blade Width^(3))/(6) to evaluate the Stress in Blade, Stress in Flat Blade formula is defined as the stress distribution in the flat blade due to action of all forces such as gas and centrifugal forces. It is observed that the maximum stress of 1.958 GPa occurs at the root section and on the pressure side of gas turbine flat blade. Stress in Blade is denoted by f symbol.
How to evaluate Stress in Flat Blade using this online evaluator? To use this online evaluator for Stress in Flat Blade, enter Force (Fm), Radius of Impeller Blade (Rb), Radius of Hub (Rh), Blade Thickness (bt) & Blade Width (bw) and hit the calculate button.