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Dynamic Pressure

Compute dynamic pressure using velocity and air density

Library

Flight Parameters

Description

The Dynamic Pressure block computes dynamic pressure.

Dynamic pressure is defined as

`$\overline{q}=\frac{1}{2}\rho {V}^{2}$`

where is air density and V is velocity.

Inputs and Outputs

InputDimension TypeDescription

First

VectorContains the velocity.

Second

Contains the air density.

OutputDimension TypeDescription

First

Contains the dynamic pressure.

Examples

See the Airframe subsystem in `aeroblk_HL20` for an example of this block.