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Hi all. I am a bit doubtful about the value of the reference area (in ANSYS fluent), I have calculated in order to match the literature's Co-efficient of Drag.! I have attached the screenshot of...
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I am working on the flow analysis of a flying object using ANSYS Fluent. I need to find out the exact amount of Lift and Drag generated by the object. Is there any way to find ?
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I would like to perform Aerodynamic and Structural analysis of various aerospace systems. I will be using the ANSYS software for performing the simulations. I want to know how shall I validate the...
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