MSC Software Corporation

The amount of effort required to close the doors of an automobile is critical to the consumer’s perception of its quality. If too high a closing velocity is required, the customer may have a negative impression of the car and the potential also exists for an unpleasant noise to be created by closing the door. The goal for most automobile manufacturers is to require a relatively low effort to close the door while at the same time meeting weather sealing and acoustic insulation requirements.

“The results of the cosimulation were provided to our customer and helped win the order to supply seals for a new model vehicle,” said Dr. H. Tuncay Yüksel, Design Director for Standard Profil. “Now that the simulation process has been developed it will be possible to simulate new seal designs in much less time and at a lower cost than physical prototyping. This will make it possible to evaluate more design alternatives to improve door closing performance as well as reduce the time and cost of the product development process.”

• Adams-Marc cosimulation helps the engineers accurately evaluate the amount of effort required to close the doors, which is critical to the consumer’s perception of its quality
• Co-simulation helps MSC customer to win order to supply seals for a new model vehicle
• Users can now simulate new seal designs in much less time and at a lower cost than physical prototyping.

Mechanical joints with fasteners are widely used for aircraft primary structures to assemble composite parts. In the case of a pin-loaded joint, stress concentration takes place on each side of the fastener leading to the apparition of local failure before the final failure of the assembly. Depends on the geometry of the joint, different failure modes may appear.

Although tests are frequently conducted to support the design of such components, the benefits of a simulation tool such as Digimat is obvious if the material modeling used is able to reproduce properly the damage behavior of the composites (unidirectional or woven reinforcement) in order to predict accurately not only the failure load but also the failure mode.

• Definition of the Progressive Failure Material model for both the UD and woven reinforced composite
• Definition of a parameterized MSC MARC finite element model to seamlessly perform a coupled analysis with Digimat.

• Good reproduction of the failure mode for the tested configuration
• Good prediction of the failure load level
• Possibility to investigate any type of geometry with confidence at no cost.

Airframes are designed to deflect in response to aerodynamic and gravitational loads during flight. These deflections in turn load the mechanisms riding on the airframe that move the primary flight control surfaces to maneuver the aircraft. The airframe manufacturer must ensure that deflections of these mechanisms at any point in the flight envelope do not affect their operation. For example, the Airbus A400M elevator is connected to the horizontal tail plane (HTP) with eight hinges that form a straight line when the wing is undeformed. Seven of these hinges are floating hinges which can float in the hinge line direction. When the HTP structure is loaded, it deforms, deforming the hinge line. The multi body simulation (MBS) model here shows the location of hinge 7 which is used to move the elevator, and the drawing below the model shows a cross-section of the hinge. The gap g2 in the drawing allows the red lug to slide on the green pin.

”The replacement of the physical A350- 1000 wing bending test with simulation of the effects of deflection on the flight controls saved Airbus about €3 million and 4 months on the certification process for the A350,” said Michael Vetter, Project Leader Multi-Body Simulation with Airbus. Most of these savings were achieved by eliminating the need to build test fixtures. Similar savings will be achieved for each future aircraft model. Airbus engineers are also working to apply this same method to other mechanical systems of the aircraft such as landing gear and passenger doors.

• Saving significant time and costs by replacing expensive physical testing with Adams simulation
• Removing the limitation on the number of different load cases and configurations that could be tested by physical test rig
• The simulation results successfully correlated with all of the tests
• These results convinced European Aviation Safety Agency(EASA) that functional testing could be replaced with Adams simulation so simulation is used to certify the A350-1000 XWB wing

The primary function of heavy duty trailer suspensions is to link the trailer to its wheels. This provides a compliant connection which protects the trailer cargo from the shock and vibration inputs developed at the road surface. In addition, the suspension must meet the customers’ expectations for usable life, and do so while being economical to manufacture. One of the challenges of trailer suspension design is that these requirements often conflict with each other. Trade-offs are often required in order to meet these performance requirements over the suspension’s entire operating range.

“We can now simulate a new suspension, in a different trailer configuration, for a specific event, in a matter of hours as compared to the days or weeks that are required with physical testing,” Dr. Patterson said. “The fact that we can change the system much faster in the simulation than on an actual trailer makes it possible to evaluate the performance of our product in more configurations, all while spending less time and money building prototypes and performing physical testing. Of course, we always run a final physical test to ensure the accuracy of our simulations. The end result is that we are able to bring products to market faster, and generate larger revenues while reducing our product development expenses.”

• Simulation results make it possible to see every aspect of suspension behavior.
• Adams results match very closely with physical test measurements on numerous occasions comparing the tire loads, component forces, and suspension performance characteristics, such as ride height change.
• Simulation provides a much better understanding of how the proposed suspension design performs than can be obtained by physical testing.
• Loads determined by the simulation are used to design fatigue tests.

Commercial applications for drones are dramatically increasing and engineers are racing to maximize payload capacity. We simulated details of the airflow pattern around a common type of commercial drone in flight to determine the pressure distribution exerted on the aircraft, lift force generated, and the cargo capacity of the drone.

The defining characteristic of a zoom lens is that its focal length can be varied. The focal length determines the angle of view — how much of the scene will be captured — and the magnification —how large individual elements will be. The shorter the focal length, the wider the angle of view and the lower the magnification. The advantage of zoom lenses over lenses with a fixed focal length is that you don’t have to change lenses to achieve a tighter or a wider composition. Most zoom lenses, particularly those designed for consumer and professional photographers, lose focus when the focal length is changed. But high-end zoom lenses, especially those designed for producing films or television, can be zoomed in and out without losing focus. This type of lens is called a parfocal lens. The first parfocal lens capable of zooming in an out while maintaining precise focus to a degree acceptable for demanding cinema production was designed and built by Pierre Angénieux in 1956, a feat for which he received an Academy award for technical excellence. Parfocal zoom lenses are very difficult to design and build. Zoom lenses generally consist of three different groups; two of them are moving together (to change focal length) and the last one independently (to focus) and one stationary group of lenses with each group comprising two of more lens elements.

With the new method proven, Ayad simulated all of the company’s zoom lenses and found the worst-case position for each lens. Now inspectors are able to inspect the tilt simply by moving the lens to this position and making the measurements. The net result is that the time needed to inspect each lens has been reduced.

• Inspection time has been reduced
• Less experienced operators can perform the inspection
• Adams simulation accurately predict worst case position

• Wind Resistance on a Sea Carrier Transporting Wood Chips
• Tank Test Simulation of Blunt Ship (Towing Condition)
• Tank Test Simulation of Blunt Ship (Self-Propulsion Condition)
• Estimation of Marine Propeller Performance in Open Water
• Predicting Marine Propeller Cavitation
• Using SC/Tetra to Estimate Ship Hull Pressure Fluctuation
• Evaluation of Small Cruising Vessel Posture using a Free Surface Analysis
• Predicting the Proportion of Discharged Air from an Aeration Tank
• Evaluation of Marine Diesel Engine Coolness
• Assessing the Capability of Water Lens Turbine for Tidal Power Generation

Evaluate the influence of aerodynamic noise and rotating stall by comparing the internal flows between different geometries of scirocco fans using SC/Tetra

The internal flow of the impeller end captured by SC/Tetra

SC/Tetra for more efficient fan product development

It takes a 450 horsepower truck with an 80,000 lb. load roughly 90 seconds to accelerate to 50 mph but the brakes must be able to stop the truck in less than 5 seconds. Air brakes are used almost exclusively in heavy-duty trucks and trailers because they offer the following advantages. First, the air they run on is free. It only needs to be compressed, cleaned, stored and distributed. The air brake circuit can be easily expanded so trailers can be coupled and uncoupled from it. Besides providing the energy required to stop the vehicle, compressed air also signals when and with how much force the brakes should be applied in any situation. Finally, air brakes can be designed with sufficient fail-safe devices to bring the vehicle safely to a stop, even in the event of an air leak. Reinforced rubber hoses deliver air from fittings on the frame to brake chambers on the axles. In a typical tandem rear suspension there are typically 8 brake hoses plus additional hoses for the power differential lock and other features for a total of 11. The hoses must be routed through a tight space and accommodate the full range of steering gear and suspension travel. The hoses are required to avoid contact with components with sharp edges that might wear the hoses, maintain a specified minimum bend radius to avoid constricting flow within the hose, and avoid axial forces high enough to pull out the hose out of the fitting.

“Simulation makes it possible to try many different positions, orientations, and clipping options early in the design phase prior to the availability of a prototype,” said Stefano Cassara, Manager Vehicle Dynamics Simulation for Navistar. “New design iterations can be evaluated in a small fraction of the time required for physical testing. The new approach makes it possible to design new hose configurations in only about two weeks. Since the design process will be carried out early and outside the critical path we should be able to bring new vehicles to market six weeks faster than in the past. Another advantage of the new approach is that we can model loading scenarios, such as braking, that cannot be duplicated on the test rig.”

• Simulation of hose routing helps reduce time to market by six weeks
• Adams predictions perfectly matched test results in each steering position
• Simulation provides a much better understanding of how to route the braking hoses to avoid contact with components with sharp edges that might wear the hoses in response to suspension and steering movement
• New Adams FE Part provided a fast and accurate way to predict the large deformation of brake hoses in Adams environment

SC/Tetra contributes to more efficient development process

Understanding flow characteristics of a valve using SC/Tetra

The Hachinohe Industrial Institute is one of the affiliated laboratories of the Aomori Prefectural Industrial Technology Research Center (hereafter the Research Center). A Prefecture is an administrative district. Japan consists of 47 prefectures. The Research Center uses HeatDesigner to help solve thermal problems for electronics. The range of applications includes scanners for food contaminants, devices for measuring the quantity of sugar and moisture in agricultural products, and inspection devices for assessing moisture and heat in coal and biomass.

Visual Basic (VB) Interface automates the evaluation of alternative vehicle height configurations