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Wingtip loadout


Lace

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Does anyone know the reason behind the doctrine change to mounting the 120s on the wingtips rather than the 9s? Logically and considering moment of inertia would it not make more sense to have the lower mass 9s on the tips?

 

 

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AIM-120 on wing-tip reduce/prevent fluttering issues.

 

 

Thanks for that, I knew it wouldn't take long! The extra mass is beneficial in that case. :thumbup:

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Thanks for that, I knew it wouldn't take long! The extra mass is beneficial in that case. :thumbup:

 

A video of the problem in this thread:

https://forums.eagle.ru/showthread.php?t=252190&highlight=wingtip

 

But causes other problems, in this thread if you are interested:

https://forums.eagle.ru/showthread.php?t=241142

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I'm sure the only reason the F/A-18 doesn't do the same is the wing hinge probably isn't strong enough to handle the additional stress.

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