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Siemens NX wing tip in flow results

Siemens NX wing tip in flow results

Siemens NX wing tip in flow results

(OP)
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i have been searching but didnt find the sollution so far. My design is a bit dfferent but you could explain it in the next example i think i can use it also for my assembly

so lets say we have a wing tip and want to do a flow analyses we desing the wing tip and the fluid domain substract one from the other and do the simulation.

When getting the results i want to see the wingtip again instead of the 'hole" . how can i do that?

wich step did i miss

kind regards

ps if i have to do something else for an assembly please let me know

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