I am trying to ascertain the weight of the V-22's entire wing assembly: right, left and center including both nacelles. But excluding the engines if possible.
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2$\begingroup$ There is a method for deriving structural wing weight from geometric data in Appendix C, Synthesis of Subsonic Airplane Design by E. Torenbeek $\endgroup$– KoyovisFeb 9, 2018 at 11:33
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