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Hello, I am currently developing a single-stage axial fan blade using the Stream Section curve. While I have been able to generate the blade surface, I am encountering challenges in understanding the camber lines produced by the Stream Section curve. Additionally, I am having trouble locating the Stream Section sample referenced by @Jörg in his post, "Axial Compressor Blade via Stream Section Curve." My objective is to generate blades by specifying beta (flow) and stagger angles. I would greatly appreciate any guidance or insights from the experts in this community. Thank you for your assistance.

Hi, I want to design an axial fan using Turbo Machine Workflow and create a fluid domain to perform CFD analysis using ANSYS Fluent. I followed the Axial Fan Tutorial available in the documentation. In this tutorial, a section of the axial fan is created along with the boundary surface. However, I do not see the fluid domain creation process. There is a tutorial video available at this https://youtu.be/9Eo44u43OFI. At 2:27 minutes, the fluid domain is shown, but the creation process is not discussed. Additionally, I tried following the tutorial in the Documentation under Tutorials/Blade Design/Centrifugal Impeller Modeling, but this option is not available for axial fan design. After designing the fan, I want to link it to CAESES Geo Engine for ANSYS Workbench and then create a workflow with Fluent. Using the parameters defined in CAESES, I aim to optimize the axial fan to achieve the required output parameters. Could you please help me create a periodic fluid domain for the axial fan? Thank you, Ruhanii Avula