## Stagnation Pressure using Mach Number Calculator

Where:- pt is the stagnation pressure (Pa) P is the static pressure (Pa) M is the Mach Number γ is the ratio of Specific Heat (J/KgK) Stagnation Pressure is the…

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# Aerodynamics Calculator

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Stagnation Pressure using Mach Number Calculator

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Pressure Coefficient Calculator

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Specific Heat Ratio Calculator

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Dynamic pressure calculator – K.Prakashbalan

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Drag polar calculator – K.prakashbalan

This category helps you to calculate the aerodynamics numerical like velocity, pressure, forces, fluid properties, etc., – WINGS OF AERO

Where:- pt is the stagnation pressure (Pa) P is the static pressure (Pa) M is the Mach Number γ is the ratio of Specific Heat (J/KgK) Stagnation Pressure is the…

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Stagnation Pressure using Mach Number Calculator

Where:- is the Static Pressure at the point at which pressure coefficient is being evaluated (Pa) is the Static Pressure in the Free-stream (Pa) is the free-stream Fluid Density (Kg/m3)…

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Pressure Coefficient Calculator

Where:- Cp is the Specific heat at constant Pressure Cv is the Specific heat at constant Volume Specific heat ratio is a Dimensionless number, It is defined as the Ratio…

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Specific Heat Ratio Calculator

Dynamic pressure(q) = 0.5*ρ*v^2 ρ - density of fluid (Kg/m^3) V - velocity (m/s) Dynamic pressure is nothing but kinetic energy per unit volume of a fluid.

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Dynamic pressure calculator – K.Prakashbalan

Cd=Cd0+K Cl^2 Drag polar is the relationship between lift on an aircraft and its drag, expressed in terms of dependence of drag coefficient on lift coefficient. It may be described…

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Drag polar calculator – K.prakashbalan