C is the chord L is the lift force generated by the wing. ρ (rho) is the air density. V is the airspeed (velocity) of the aircraft relative to the air N is Normal force
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The axial force coefficient (CA) is a dimensionless quantity used in aerodynamics to describe the axial force acting on a body, such as an airfoil or wing, due to the fluid flow. It is one of the force coefficients used to understand the aerodynamic behavior of bodies in fluid flows. CA = Axial force coefficient
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The induced drag coefficient is a measure of the drag caused by the generation of lift on a wing or an airfoil. It is related to the lift coefficient, the aspect ratio, and the efficiency factor of the wing or airfoil. Cdi is the induced drag coefficient Cl is the lift coefficient pi is the
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The aspect ratio of a wing is the ratio of its span to its mean chord. AR = b2/S.
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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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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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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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In aerodynamics, dynamic pressure (also known as “q” or “q∞”) is a measure of the kinetic energy of a moving fluid, such as air, per unit volume. It is a fundamental concept used to understand the forces acting on an object (like an aircraft) as it moves through the fluid. q is the dynamic pressure
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The coefficient of drag (Cd) is a dimensionless parameter that quantifies the resistance an object experiences as it moves through a fluid, such as air. It is a crucial factor in understanding the aerodynamic performance of various objects, including aircraft, rockets, cars, and other vehicles. Where: Cd is the drag coefficient, D is the drag
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The coefficient of lift is a dimensionless quantity used in aerodynamics to describe the lift generated by an airfoil, wing, or other aerodynamic surface. It provides a standardized measure of the lift produced by the surface relative to its size, shape, and the flow conditions. The coefficient of lift helps engineers and researchers compare and
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