COSMOS FloWorks Wind Tunnel Simulation

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Presentation transcript:

COSMOS FloWorks Wind Tunnel Simulation ME143 Fall 2006 J. Cho B. Wilson

COSMOS FloWorks Tutorial Build a part Car Body Wing Shape Entire Aircraft Select Simulation Parameters Fluid Fluid Velocity Run Simulation View Results

COSMOS FloWorks Tutorial Draw a part in SolidWorks

COSMOS FloWorks Tutorial Execute FloWorks Add-In Tools > Add-Ins

COSMOS FloWorks Tutorial Start New Simulation FloWorks > Project > Wizard

COSMOS FloWorks Tutorial Set Simulation Units System

COSMOS FloWorks Tutorial Choose Flow Type Internal: Pipes, Ducts, etc… External: Flow over surfaces

COSMOS FloWorks Tutorial Choose Fluid

COSMOS FloWorks Tutorial Set Surface Conditions

COSMOS FloWorks Tutorial Set Initial Conditions Flow Velocity and Direction Initial Pressure and Temperature

COSMOS FloWorks Tutorial Set Simulation Accuracy More Accuracy = More Simulation Time

COSMOS FloWorks Tutorial Size the Computational Domain FloWorks > Computational Domain

COSMOS FloWorks Tutorial Run Solver FloWorks > Solver > Run

COSMOS FloWorks Tutorial Wait for Solution to be Computed Depending on geometry and accuracy, simulation time can be several hours

COSMOS FloWorks Tutorial Solver Window Completed Simulation

COSMOS FloWorks Tutorial Insert Flow Trajectories Results > Flow Trajectories > Insert Export Images and Video

COSMOS FloWorks Tutorial Results Image

COSMOS FloWorks Tutorial Results Animation Click image to Animate

Wind Tunnel Comparisons Air Foil Horizontal Inclined 20 degrees 1969 Chevrolet Camaro 30 mph 60 mph

Wind Tunnel Comparisons Airfoil Image (Horizontal Position)

Wind Tunnel Comparisons Airfoil Animation (Horizontal Position) Click image to Animate

Wind Tunnel Comparisons Airfoil Results (Horizontal Position) Low pressure zone on top of foil produces lift. Laminar air flow over entire profile.

Wind Tunnel Comparisons Airfoil Image (20° Incline)

Wind Tunnel Comparisons Airfoil Animation (20° Incline) Click image to Animate

Wind Tunnel Results Airfoil Results (20° Incline) 20° incline increases surface area. More pressure is developed at bottom of airfoil, producing higher lift capabilities for take offs and in-flight maneuverability.

Wind Tunnel Comparisons 1969 Chevrolet Camaro (30mph)

Wind Tunnel Comparisons 1969 Chevrolet Camaro (30mph) Click image to Animate

Wind Tunnel Comparisons 1969 Chevrolet Camaro (60mph)

Wind Tunnel Comparisons 1969 Chevrolet Camaro (60mph) Click image to Animate

Wind Tunnel Results 1969 Chevrolet Camaro Results Front vehicle geometry (front spoiler) Improves aerodynamics Rear spoiler provides a downward force Keeps vehicle on ground at high speeds

Conclusion Cosmos FloWorks All simulation data is exportable in Excel format or preformatted “Word” documents. Flow profile are easily examined for turbulence. Multicolored pressure lines easily display pressure differentials. All fluid properties and flow parameters are adjustable. Fluid information is included in program.