Hi all,I'm working on building an aerodynamic database for a VTOL tail-sitter that relies heavily on propeller slipstream for attitude control during ascent. It appears that VSPAERO can handle propeller-blown wing simulation during non-static condition (free-stream velocity is not zero) and some validation data was published in a recent paper. However, I wonder if it is possible to perform the same simulation but with zero free-stream velocity as it would be during vehicle hover.I'd imagine that I can set Vinf to be zero and cut off any Cl on wing sections that are not in the propeller slipstream, but I'm not quite sure if this is the proper way to go.--
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Dear Mr. McDonald , Is it possible to email me any openvsp model so i can play with it ? or is there a link i can download it from? i try to post my email here but the system deleted right away, so vincent1500 at 126 dot com is my email.
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