Calculate nozzle exit velocity V = Cv·√(2gh) and thrust F = ρ·A·V². Velocity coefficients Cv = 0.97-0.99 for well-designed nozzles. Converging-diverging nozzles for supersonic flow with critical pressure ratio.
2D stress state at a point. All stresses in MPa.
Enter the values for the patient or scenario you are assessing. Calculate nozzle exit velocity V = Cv·√(2gh) and thrust F = ρ·A·V². Velocity coefficients Cv = 0.97-0.99 for well-designed nozzles. Converging-diverging nozzles for supersonic flow with critical pressure ratio. Use the nozzle velocity result to inform your clinical assessment.