CAESIM Simulation Platform

A D V A N C E D C O M P U T E R - A I D E D E N G I N E E R I N G S O L U T I O N S

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E X P L O R E U N L I M I T E D S I M U L A T I O N P O S S I B I L I T I E S !

C O M P U T E R - A I D E D E N G I N E E R I N G S I M U L A T IO N P L A T F O R M

F L U I D F L O W, H E A T T R A N S F E R, A N D M U L T I - P H Y S I C S

S I D E V I E W

Vortex Structures

F R O N T V I E W

Pressure Fields

T O P V I E W

Transient Motion

3D W I N G F L A P P I N G with F S I

Computational fluid dynamics simulations were performed using an unsteady compressible flow solver (STORM) to determine the acoustic characteristics of a flexible membrane flapping wing for a Coconut Rhino beetle at hovering and forward flight conditions. CAESIM includes advanced capabilities for aerodynamic analysis of moving bodies in turbulent compressible flows, including rigid-body and flexible membrane fluid-structure interactions.

CAESIM simulates 3D transient wing flapping motion with compressibility and fluid-structure interaction (Funding: UOH - J. Allen)

3 D F L I G H T

Vorticity

I S O - V I E W

Pressure Waves

S T A T I C V I E W

Streamlines

CAESIM Applications

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S I D E V I E W

F R O N T V I E W

T O P V I E W

3D W I N G F L A P P I N G with F S I

3 D F L I G H T

I S O - V I E W

S T A T I C V I E W

L I C E N S E I N F O R M A T I O N

CAESIM Student License

CAESIM Standard License

CAESIM Advanced License

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