Thrust

The thrust report integrates the momentum flux and the pressure force over a specified boundary or derived part.

The thrust report is represented in the simulation tree by a node, which has its own properties but is subject to the report node’s pop-up menu. This report is active for flow models.

The thrust is computed as:

Figure 1. EQUATION_DISPLAY
T=fρfvfvfaf+f(pfpatm)af
(468)

where ρf is the fluid density, v is the velocity vector, pf is the exit pressure, patm is the atmospheric pressure, and af is the surface area vector of the face.

The governing equation that is being solved is the reaction force at the boundary:

Figure 2. EQUATION_DISPLAY
T=ρvvds+(ppatm)ds
(469)
This equation is illustrated in the following diagram:

Thrust Report Properties

Direction

Specifies the Cartesian vector that is used to compute the scalar product with the reaction thrust vector. This lets you calculate the component of the thrust that is acting in a particular direction.

Atmospheric Pressure

The atmospheric pressure for the computation of Eqn. (468).

Coordinate System

A list of coordinate systems that this report can use.

Parts

A list of parts that are used as the source for this report. Opens the in-place part selector for editing. The (property customizer) button activates a modeless version of the selector dialog (it lets you interact with other portions of the workspace).

Units

Units that are used for specifying the quantity.

Thrust Report Expert Properties

Representation

Selects a representation. Additional selections appear as representations that are added to the simulation.

Smooth Values

When this property is activated, the report is calculated using node (interpolated) values of the chosen quantity rather than cell values.