Author name: Ravula Nikhil Reddy

Lift-Off Velocity (VLOF) Calculator

Lift-Off Velocity (VLOF) is the minimum speed an aircraft must reach during the takeoff roll to become airborne. It represents the speed at which the lift generated by the aircraft’s wings becomes equal to the weight of the aircraft, allowing it to overcome gravity and lift off the ground. The formula to calculate Lift-Off Velocity […]

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Skin Friction Coefficient For Turbulent Calculator

Skin Friction Coefficient (Cf) is a dimensionless quantity that characterizes the frictional resistance between a fluid and a solid surface in a flow. It is used in fluid dynamics to quantify the effects of viscous forces on the flow over a surface. Turbulent flow is a type of fluid motion characterized by irregular and chaotic

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Skin friction Coefficient for Laminar Calculator

The skin friction coefficient (Cf​) is a dimensionless quantity that characterizes the frictional resistance of a fluid flow over a surface. The skin friction coefficient is often used in the context of boundary layer analysis. For laminar flow over a flat plate, the skin friction coefficient can be estimated using the following formula: where: Cf​

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Dynamic pressure in terms of Mach Number calculator

Dynamic pressure (q) is a term in aerodynamics that represents the kinetic energy per unit volume of a fluid due to its motion. As an aircraft’s speed increases, the dynamic pressure on its surfaces also increases. In terms of the Mach number (M), which is the ratio of the speed of an object to the

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Turn radius (R) in level coordinated flight Calculator

The turn radius (R) in aviation refers to the horizontal distance from the center of a turn to the path followed by the aircraft during a coordinated turn. As the load factor increases, the turn radius decreases, and vice versa. This critical parameter, influenced by factors like airspeed and bank angle, is essential for understanding

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Stall speed in straight and level flight Calculator

The Stall speed refers to the minimum airspeed at which an aircraft can maintain controlled flight without entering a stall. A stall occurs when the critical angle of attack is exceeded, leading to a disruption in the smooth airflow over the aircraft’s wings. The stall speed increases with an increase in load factor. The relationship

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Side force coefficient Calculator

The side force coefficient (Cy​) is an aerodynamic parameter that describes the generation of lateral (side) force on an aircraft in response to sideslip. Sideslip occurs when the aircraft’s longitudinal axis is not aligned with the relative wind. The side force (Y) is the aerodynamic force acting perpendicular to the aircraft’s longitudinal axis. The formula

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