Aerodynamics Calculator

Boost your aerodynamic endeavors with the online aerodynamics calculator by ToDo Calculator. Tailored for aerospace engineers, researchers, and enthusiasts, this versatile tool facilitates a myriad of aerodynamics calculations. Leveraging the robust capabilities of ToDo Calculator, it delivers precise solutions across various parameters, from airfoil analysis to lift and moment calculations. With its intuitive interface, this calculator demystifies complex aerodynamic computations, empowering both professionals and students alike. Whether you’re crafting aircraft or delving into fluid dynamics, this resource accelerates your aerodynamics analysis, ensuring optimal performance in aerospace projects.

Lift coefficient for the airfoil section located at arbitrary spanwise station Calculator

The lift coefficient (Cl) for an airfoil section located at an arbitrary spanwise station represents the dimensionless measure of the lift generated by that specific section of the airfoil.  Local section lift slope (a0) in per rad Effective angle of attack at the spanwise station y₀ (αeff(y₀)) in rad Zero-lift angle of attack (αL=0) in […]

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Induced angle of attack for small angles at the arbitrary spanwise station Calculator

The induced angle of attack at an arbitrary spanwise station refers to the angle of attack that is created at a specific location along the span of an aircraft’s wing due to the presence of downwash from neighboring sections of the wing. In other words, it represents the effective angle of attack experienced by a

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Induced angle of attack at the arbitrary spanwise station Calculator

The induced angle of attack at an arbitrary spanwise station refers to the angle of attack that is created at a specific location along the span of an aircraft’s wing due to the presence of downwash from neighboring sections of the wing. In other words, it represents the effective angle of attack experienced by a

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Downwash distribution along the y axis for a single horseshoe vortex Calculator

The downwash distribution along the y-axis for a single horseshoe vortex can be described using potential flow theory. A horseshoe vortex is often used as a simplified model to represent the vortical flow structure generated by the wingtip or wingtip vortex system. In this case, we’ll consider a horseshoe vortex where the vortex elements are

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Cartesian coordinate of y-axis for the doublet two Calculator

Cartesian coordinate systems, the y-coordinate (y2) for the doublet refers to the vertical position of the doublet source (or sink) along the y-axis. The y-axis is one of the two perpendicular axes in a Cartesian coordinate system, typically representing the vertical direction. For a doublet located in a Cartesian coordinate system with its center at

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Cartesian coordinate of y-axis for the doublet one Calculator

Cartesian coordinate systems, the y-coordinate (y1) for the doublet refers to the vertical position of the doublet source (or sink) along the y-axis. The y-axis is one of the two perpendicular axes in a Cartesian coordinate system, typically representing the vertical direction. For a doublet located in a Cartesian coordinate system with its center at

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Cartesian coordinate of y-axis for the doublet one Calculator

Cartesian coordinate systems, the y-coordinate (y1) for the doublet refers to the vertical position of the doublet source (or sink) along the y-axis. The y-axis is one of the two perpendicular axes in a Cartesian coordinate system, typically representing the vertical direction.  Cartesian coordinate for y axis for doublet one (y1)  r1 is the radial

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Radial distance of doublet two Calculator

The radial distance of a doublet refers to the perpendicular distance from the doublet source (or sink) to a specific point in the flow field. The doublet is a theoretical construct used to model certain flow patterns, and its radial distance is an important parameter when analyzing its influence on the surrounding fluid.   r2 is

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Radial distance of doublet one Calculator

The radial distance of a doublet refers to the perpendicular distance from the doublet source (or sink) to a specific point in the flow field. The doublet is a theoretical construct used to model certain flow patterns, and its radial distance is an important parameter when analyzing its influence on the surrounding fluid.  r1 is

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