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Virtual Twins for Rail Simulation

Revolutionize rail safety, fuel efficiency and reliability of your rail operations through aerodynamics and vehicle dynamics simulation using virtual twin technology.

EBooks

Virtual Twins for Rail Simulation
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Embracing Transformation

Industry experts use MODSIM to streamline product design by breaking down silos, validating designs early, optimizing parts, and fostering better collaboration.

EBooks

Embracing Transformation
Numerical and Experimental Investigation of Flow Confinement Effects on UAV Rotor Noise

The primary objective of the present study is to investigate the impact of the recirculating flow that develops inside a closed, hemi-anechoic test chamber on the noise generation mechanisms of a drone rotor operated under static thrust conditions. To that end, Lattice-Boltzmann simulations are conducted for both an idealized, semi-infinite free-field and a confined, hemianechoic domain that models the test chamber, with the latter validated against experimental measurements. Comparison between simulations reveals a significant increase in rotor noisedue to confinement, up to 5 dBA in overall sound pressure level depending on microphone location, with negligible impact on aerodynamic performance. Blade-strip and beam-forming source identification techniques are utilized to determine those sound-generation mechanisms responsible for the increase in rotor noise. Leading-edge interactions between the vortical structures convected by the recirculating flow and the rotor’s blades are demonstrated to be directly responsible for the generation of unsteady loads that lead to significantly higher bladepassing frequency harmonic peaks. A small enhancement of the high-frequency self-noise contribution is also observed, whereas blade-tip vortex dynamics are largely unaffected by confinement so that the contribution of blade-vortex interaction noise is negligible.

Tech Notes

Numerical and Experimental Investigation of Flow Confinement Effects on UAV Rotor Noise
Community Noise of Urban Air Transportation Vehicles

This paper describes computational work ows for the evaluation of the acoustic environmental impact of vertical take-o and landing vehicles. An operational scenario of a vehicle undertaking an approach maneuver over a at terrain is considered. The aeroacoustic sources are predicted by using the high-fidelity CFD solver SIMULIA PowerFLOW based on the Lattice-Boltzmann/very-large-eddy-simulation method. An integral approach based on the Ffowcs-Williams and Hawkings analogy is used to compute the noise on a hemisphere centered around the vehicle. Finally, the on-ground noise footprint is computed by using the hemisphere noise extrapolation approach. In view of future trajectory/maneuver optimization studies, different trimmed trajectories are considered in order to show the effect of both the aero-mechanical setting of the vehicle and its instantaneous position on the perceived noise levels along a fly-over event. Trajectories are described by a time sequence of waypoints, vehicle pitch angle, tilt angles of the propulsion units and rotational speed of the rotors.

Tech Notes

Community Noise of Urban Air Transportation Vehicles
Turbofan Broadband Noise Prediction Using the Lattice Boltzmann Method

The present work describes a numerical reproduction of the 22-in source diagnostic test fan rig of the NASA Glenn Research Center. Numerical flow simulations are performed for three different rotor/stator configurations and one rotational speed, representative of an approach operating condition, by using the lattice-Boltzmann solver PowerFLOW. The full stage and nacelle geometries are considered, and results are compared to available measurements. Tripping the rotor blades results in a slightly more accurate noise prediction as a consequence of amore accurate prediction of the velocity fluctuations in the rotor wake over the whole blade span. Fourier circumferential analyses are performed for an intake and a bypass duct section with the intent of explaining the origin of some tonal noise components and comparing the present results to available literature results. Finally, the effects of adding an acoustic treatment in the intake is shown by directly resolving the unsteady flowfield in a single-degree-offreedom honeycomb layer.

Tech Notes

Turbofan Broadband Noise Prediction Using the Lattice Boltzmann Method
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Simulation of Aircraft Aeroacoustics | Dassault Systèmes

Watch the replay to discover how aeroacoustic simulations are performed for aircraft using the PowerFLOW software. Specific applications covered include noise generated by landing gear and high-lift configurations.

E-seminar

Simulation of Aircraft Aeroacoustics | Dassault Systèmes
On demand
Electric Drive Engineering | Dassault Systèmes

Watch the replay to learn how multi-disciplinary workflows can be used to simulate the complexity of an electric drive and evaluate multiple design variants quickly and efficiently.

E-seminar

Electric Drive Engineering | Dassault Systèmes
On demand

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SIMULIA Self Learning

We provide hundreds of self-learning modules so you can continue to learn at your convenience

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Read the SIMULIA blog on the latest news and innovations from our experts.

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Unified Modeling and Simulation

Exploring how we do science-based modeling and simulation, and how new paradigms in this field are delivering next-generation product design systems with modeling and simulation at their core.

Article

Unified Modeling and Simulation
Protecting Buildings Against Lightning Strike and EMP: Electromagnetic Simulation Can Help

It only takes the Wi-Fi to cut out for an hour for us to realize how dependent we are on being connected. Much of our modern lifestyle is dependent on digital connectivity and infrastructure, so it becomes crucial that the buildings that provide that connection and store our data, such as data centers, are protected against unintentional or intentional electromagnetic (EM) events.

Article

Protecting Buildings Against Lightning Strike and EMP: Electromagnetic Simulation Can Help

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