August 2023

Dynamic pressure for wedge simplified Calculator

In the context of a wedge in aerodynamics, dynamic pressure (q1​) is a measure of the kinetic energy per unit volume of the fluid flowing around the wedge shape. It represents the pressure increase that would occur if the fluid were brought to a complete stop, converting all of its kinetic energy into pressure energy. 

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Vertical force component acceleration due to gravity calculator

In flight mechanics, the “vertical force component” refers to the net force acting vertically on an aircraft. This force is a result of the balance between the aircraft’s weight and the lift generated by its wings. It determines whether the aircraft is climbing, descending, or maintaining level flight in the vertical direction. Z = mz

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Wedge drag coefficient Calculator

The drag coefficient for a wedge is a dimensionless quantity that characterizes the aerodynamic drag of a wedge-shaped object moving through a fluid. It’s a valuable parameter in aerodynamics and is used to quantify how efficiently a wedge shape interacts with the fluid flow.  Drag coefficient (cd) Wedge angle (𝜃) in rad Pressure over the

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Vertical force component (net force acting vertically on the aircraft) calculator)

The vertical force component in flight mechanics, also known as the “net vertical force,” refers to the resultant force acting in the vertical direction on an aircraft. It’s the difference between the lift force and the weight force. The vertical force component is a key factor in determining the aircraft’s vertical equilibrium and its behavior

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Drag on a unit span of the wedge with respect to chord length Calculator

The “drag on a unit span of the wedge,” often denoted as D′, refers to the aerodynamic force acting on a unit span (usually 1 meter) of a wedge-shaped object due to the airflow around it. This force is known as drag, and D′ specifically quantifies the drag force per unit span length.  Drag on

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Vertical force component calculator

In flight mechanics, the “vertical force component” refers to the net force acting in the vertical direction on an aircraft. This force is essential for maintaining the aircraft’s vertical equilibrium during flight. The vertical force component is a result of the interplay between the aircraft’s weight and the lift generated by its wings. Z =

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Total pressure across the shock in a supersonic flow Calculator

The total pressure across a shock wave in a supersonic flow, denoted as p0,2​, is the sum of the static pressure and the dynamic pressure after the flow has passed through the shock. It represents the total energy of the flow, which includes both pressure energy and kinetic energy due to the flow velocity.  Total

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