Researchers at the Division of Applied Biomedical Engineering at the Penn State College of Medicine have been using CAESES in combination with CONVERGE as a CFD Integrated Optimization Platform for the development of safer and more efficient ventricular assist devices.
Within the framework of the project “Transitioning to Low Carbon Sea Transport” (TLCSeaT), focusing on the new-build of a sail assisted general cargo and island supply vessel for the Republic of Marshall Islands (RMI), CAESES has been used to create a parametric design and calculation environment that can be used for the evaluation of different design options during the vessel’s concept and early design phases.
Shape morphing allows you to easily import an existing geometry model and reshape your design with regards to the flow and structural performance. Read this blog post for a comparison of the different morphing approaches in CAESES 5 and how it offers intuitive and exact shape modifications that can be set up in a matter of minutes.
There is no excerpt because this is a protected post.
In this blog post, problematic dynamic instabilities in the operation of the baseline poppet valve were investigated and effectively solved by setting up an automated workflow with CAESES® and SimericsMP®.
The present case study investigates a hypothetical intake duct geometry for a TBCC propulsion system, which channels high-speed air from the freestream into the engine and converts the dynamic energy into high pressure by making use of a series of compression shocks.
This academic blog post describes how CAESES was used to design a parametric turbopump inducer geometry in conjunction with Ansys CFX.
This blog post deals with the improvement of the design of the internal layout of oil tankers targeting safety and economic feedback and considering the incorporated uncertainty.
The present work explores novel sCO2 axial turbine designs for waste heat recovery (WHR) applications based on a 10 MW case study. A Kulfan Class Shape Transformation (CST) for 2D axial blade profile design is employed, and considerations are undertaken for aerodynamic efficiency and mechanical stresses.
There is no excerpt because this is a protected post.