Jet-Engine-Fan-CFD-Simulation-ANSYS-CFX-Pressure-Contor-FetchCFD.jpg size: 0.176442 MB
Jet-Engine-Fan-CFD-Simulation-ANSYS-CFX-Pressure-Contor-Side-View-FetchCFD.jpg size: 0.082267 MB
Drone-Simulation-ANSYS-CFX-Simulation-File-FetchCFD.rar size: 29.045648 MB
Embed Code for Jet Engine Fan CFD Simulation
Copy the embed code below to include this project on your website:
Jet engine fan cfd simulation
NoAI: This project, including models, simulations, images, and descriptions, may not be used within datasets, during the developmental process, or as inputs for generative AI tools.
About the Jet Engine Fan CFD Simulation Project
Transient simulation of turbofan using ANSYS CFX. Turbofan also known as fanjet belongs to the airbreathing jet engine type that is commonly used in propulsion system of an aircraft. Around 4.5 Million cells and SAS turbulence model are used in this simulation with a simulation time of around 0.3 s. Simulation files are also attached for free download. Turbofan CAD model is made by Shreyash Kudve (https://grabcad.com/shreyash.kudve-1)
Statistics
54 Downloads
4 Likes
11924 Views
0 Comments
4 Files
29 MB Project Size
May 16th, 2018 Uploaded
Share
Share Tweet Pin Share Share Post ShareWatch Related Video on Jet Engine Fan CFD Simulation Project
Discover insights and details about the "Jet Engine Fan CFD Simulation " project in this informative video. Gain a deeper understanding of the design, process, and application directly from our experts.
Video | Jet Engine Fan CFD Simulatio...
Max Payne
295 Projects
468 Likes
8740 Downloads
Tags
Simulation, Jet Engine Aerospace, Aircraft propulsion, Fanjet, Airbreathing jet engine, turbofan, Jet Engine Fan
Categories
Sponsored Ad from FindingDIY
Related Projects
Sign up to join the conversation about Jet Engine Fan CFD Simulation
Post a comment! Share insights on Jet Engine Fan CFD Simulation , ask questions, and connect with other users. Whether you're curious about the 3D model, fluid simulation, or finite element analysis, your comments enrich the conversation.
No responses added yet.
