Thermal-Analysis-Orion-Spacecraft-Directional-Heat-Flux-Contour-FetchCFD-Image.jpg size: 1.145098 MB
Thermal-Analysis-Orion-Spacecraft-Geometry-FetchCFD-Image.jpg size: 0.997543 MB
Thermal-Analysis-Orion-Spacecraft-Temperature-Contour--FetchCFD-Image.jpg size: 1.147843 MB
Thermal-Analysis-Orion-Spacecraft-Total-Heat-Flux-Contour-FetchCFD-Image.jpg size: 1.167208 MB
Thermal-Analysis-Orion-Spacecraft-Mesh-FetchCFD-Image.jpg size: 3.286763 MB
Thermal-Analysis-Orion-Spacecraft-ANSYS-Workbench-Project-Coarse-Mesh-FetchCFD-File.wbpz size: 26.517563 MB
Thermal Analysis Orion Spacecraft
NoAI: This model, simulation, images, or project may not be utilized within datasets, during the developmental process, or as inputs for generative AI programs.
Thermal analysis is the study of properties of materials with respect to the change in temperature. In thermal analysis simulations the physical or chemical properties of a substance are analyzed when it is heated, cooled, or held at a constant temperature with the help of a computer. Thermal Analysis is important in a number of industries such as composites, pharmaceuticals, polymers, petroleum, foods, inorganic and organic etc. This project is about the thermal analysis of Orion spacecraft. Software used in this analysis is ANSYS Workbench. Boundary conditions are Temperature 9K C with convection 22 C and % W/m²C. Mesh consists of around 69k elements. Ansys workbench project (.wbpz) file is attached. Please like and share thanks!!
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46 MB Project Size
July 27th, 2021 Uploaded
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