Author name: Bhagiya Prasad

Pressure Co-efficient Calculator

The pressure coefficient, denoted as “Cp,” is a dimensionless parameter used in fluid dynamics and aerodynamics to describe the pressure distribution around an object immersed in a fluid flow. It is a normalized measure of the pressure at a particular point on the object relative to the freestream dynamic pressure of the fluid.  Cp: Pressure

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Skin friction coefficient Calculator

The skin-friction coefficient, denoted as “cf” is a dimensionless quantity used in fluid dynamics to characterize the frictional drag experienced by a fluid flowing over a solid surface.       cf- Skin-friction coefficient τ- Skin friction or shear stress acting on the surface of the body q∞- Dynamic pressure of the freestream flow

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Pitching Moment Co-efficient Calculator

The pitching moment coefficient (CM) is another important dimensionless quantity used in aerodynamics to describe the pitching moment acting on a body, typically an airfoil or wing, in a fluid flow. It is a crucial parameter in understanding the stability and control characteristics of an aircraft. CM = Pitching moment coefficient M = Actual pitching

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Normal force co-efficient Calculator

In aerodynamics, the normal force coefficient (CN​) is a dimensionless parameter used to describe the lift or downforce generated by an object, such as an airfoil, wing, or any other body moving through a fluid, typically air. The normal force refers to the force that is perpendicular to the freestream flow direction. ​ CN​ is

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Drag co-efficient with dynamic pressure Calculator

The coefficient of drag (CD​) is a dimensionless quantity used in aerodynamics to describe the amount of drag generated by an object as it moves through a fluid, such as air. CD​ is the drag coefficient, D is the drag force acting on the object, q∞​ is the dynamic pressure of the freestream flow (far

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Lift co-efficient with dynamic pressure Calculator

The lift coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. The lift coefficient is used to determine the lift generated by an airfoil or other lifting body at a given angle of attack. L

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