Scissor Lift Wind Load Analysis

Scissor Lift Wind Load Analysis
Analysis: 
CFD

Although usually not necessary, given its high-value electronics equipment, a detailed CFD wind-load analysis was done on this commerical scissor lift. 

Wind load forces from this CFD consulting study were then used to calculate stability loads for a safe operating range under human operation.. The CFD study allowed the client to give a wind rating with high confidence. It additionally saved the client thousands of dollars since they did not need to do physical wind tunnel testing.   

The model was built with client supplied CAD geometry (see Figure 1). 

The tipping force was calculated at varying extension heights.  The computational fluid dynamics (CFD) analysis was run to determine the force on the structure at varying wind speeds.  These forces were verified against wind load calculations from ASCE 7-02, Minimum Design Loads for Building and Other Structures.  A typical calculation table can be seen below in Table 1.

Typical CFD simulation results can be seen in the figures below.  Air flow traces and static pressure can be seen in Figure 2 and a typical velocity magnitude plot can be seen in Figure 3

Keywords:  CFD Consulting, Computational Fluid Dynamics, Fluid Mechanics, ASCE Wind Load Analysis, ASCE 7-02, Stability Analysis, Tipping Analysis, US Air Force, 

Table 1: Typical CFD Wind Load calculation table

Table 1: CFD Wind Load Calculation Table. This provides the total wind load on the structure as a function of wind speed.

Figure 1: The simplified geometry based on supplied CAD models

Figure 1: The simplified geometry based on supplied CAD models. This geometry was used for the CFD analysis to calculate the total wind load on the structure. The loads from the CFD model correlated well with loads calculated per ASCE 7-02, Minimum Design Loads for Building and Other Structures

CFD simulation air flow traces and static pressure.

Figure 2: This image show the CFD air flow particle traces and a contour of static pressure over the structure. 

CFD wind velocity contour plot over scissor-lift

Figure 3: In this image, the CFD wind velocity is contoured over a section cut through the CFD model. 

In collaboration with our CFD consulting engineers, the client was able to demonstrate that the scissor-lift would be stable under all normal operating conditions. Based on these numerical results, the scissor-lift was signed off to operate on the US Air Force base without physical testing.

Our Partners

Siemens PLM Software
Livermore Software Technology Corporation
Applied CAx
Sherpa Design