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The inherent risk in new medical product development can be mitigated through a deeper understanding of the design properties and functions achieved through modeling and simulation. Biomedical device design is facing increasing product complexity while prototype building and testing can take months, especially when clinical trials are concerned. This Webinar will show the latest advancements in computational modeling and simulation and highlight new tools available to help improve things like bench top tests and in vitro and in vivo tests. New methods to better handle scale-up challenges and...
Mixing Simulation with Ease: Automating the Simulation Set-up Process
Poor mixing can result in the loss of millions of dollars within the chemical, pharmaceutical and many allied industries. Computational Fluid Dynamics (CFD) simulation is used to answer the numerous challenges that cannot be solved by analytical or experimental methods. This is especially important in the design and scale-up phases of process development. A common hurdle in performing simulation mixing for engineers who are new to simulation is the significant amount of time required to set up geometry, meshing and adequate physics. Even for experienced simulation experts, creating both...
CD-adapco China诚邀您参加“使用流体固体相互作用 (FSI) 扩展多学科分析领域”网络研讨会! 本次网络研讨会将展示出单个集成用户界面内的模拟如何通过多种技术应用于执行FSI分析,包括利用突破性的新有限元求解器。
The performance of the Standard Cirrus glider is simulated using a Computational Fluid Dynamics code, solving the incompressible Navier-Stokes equations for steady flow. To calculate the transitional boundary layer flow a correlationbased transition model is used. It is found that the numerical model is able to predict the performance of the Standard Cirrus well. The simulations using the transition model are found to improve the results compared to fully turbulent simulations, except for the region of the stall. The best in-flight measured glide ratio for the Standard Cirrus is 36.5 at 94.5...
Computational Fluid Dynamics is routinely used in clearance of stores for carriage and release from aircraft in the transonic range of flight. A well-known validation case is modelled in this study, for which aerodynamic loads have been compared with wind tunnel experimental data by other authors. In this study, having validated the numerical model, we apply more recent methodologies from flow dynamics to study the detailed flow field in the region of the store fins.
Double Overset Store Separation Analysis
Animation showing separation of two stores using double overset mesh
Validation of an Unstructured Overset Mesh Method for CFD Analysis of Store Separation
Stage separation of a Delta Launch Vehicle using Overset Mesh. Animation shows the pressure gradients along a center plane section as the stages separate.
The Crescendo model is a simplified version of a helicopter turbine. With the use of Surface Wrapper and the CHT capabilities of STAR-CCM+, engine cooling of the model can be accurately analyzed. Image shows thermal contours on the turbine and the polyhedral mesh on the surface.