Aerospace Blockset™

Discrete Wind Gust Model - Generate discrete wind gust

Library

Environment/Wind

Description

The Discrete Wind Gust Model block implements a wind gust of the standard "1-cosine" shape. This block implements the mathematical representation in the Military Specification MIL-F-8785C [1]. The gust is applied to each axis individually, or to all three axes at once. The user specifies the gust amplitude (the increase in wind speed generated by the gust), the gust length (length, in meters, over which the gust builds up) and the gust start time.

The Discrete Wind Gust Model block can represent the wind speed in units of feet per second, meters per second, or knots.

The following figure shows the shape of the gust with a start time of zero. The parameters that govern the gust shape are indicated on the diagram.

The discrete gust can be used singly or in multiples to assess airplane response to large wind disturbances.

The mathematical representation of the discrete gust is

where V_m is the gust amplitude, d_m is the gust length, x is the distance traveled, and V_wind is the resultant wind velocity in the body axis frame.

Dialog Box

Units

Define the units of wind gust.

Units	Wind	Altitude
Metric (MKS)	Meters/second	Meters
English (Velocity in ft/s)	Feet/second	Feet
English (Velocity in kts)	Knots	Feet

Gust in u-axis

Select to apply the wind gust to the u-axis in the body frame.

Gust in v-axis

Select to apply the wind gust to the v-axis in the body frame.

Gust in w-axis

Select to apply the wind gust to the w-axis in the body frame.

Gust start time (sec)

The model time, in seconds, at which the gust begins.

Gust length [dx dy dz] (m or f)

The length, in meters or feet (depending on the choice of units), over which the gust builds up in each axis. These values must be positive.

Gust amplitude [ug vg wg] (m/s, f/s, or knots)

The magnitude of the increase in wind speed caused by the gust in each axis. These values may be positive or negative.

Inputs and Outputs

Examples

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

Reference

U.S. Military Specification MIL-F-8785C, 5 November 1980.

See Also

Dryden Wind Turbulence Model (Continuous)

Dryden Wind Turbulence Model (Discrete)

Von Karman Wind Turbulence Model (Continuous)

Wind Shear Model

Direction Cosine Matrix to Wind Angles

Dryden Wind Turbulence Model (Continuous)