Statics Review Problem - simplified wing strut problem

Statics Review Problem - simplified wing strut problem - S...

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Unformatted text preview: S {ZAW-cg @VI-ébf 77m U6 M V2. Note Title 8/14/2007 Cad/ch '- A $IMA.“ air-Puma ts nit?! w'd'L o~ S‘l'ru'l‘- Erma, w;'~j 0‘5 Skowlfl- 15 11") +0 11‘8 +0 sccec‘l- 0- ?Oia‘l,‘ Far fie S+Nlt +0 Connecl- To W WIM Spar. TR; Maximum wclflL‘l‘ of W plane is 900 MA it Ska“ I'Je aide *D \JWLSM walked-lens 0F 55, Eff: Comrressgvt fine In Loin} S'l'mf as a unchon o-F aTrMwaen‘t (ocad‘l'ovx,c.. - Ph_§to Courtgsy of Manhias‘GIutz-I_ ' 6; LMA=SOoleZ=ZooolL 2 Final: Tlnc 'Ercc: lv\ +L\e clijMA/ S‘W‘U7L1 1.? /2 Ew- wa elk-VFem'L S*wu‘\ A-fiacLWh-F POI-n+5 ...
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Statics Review Problem - simplified wing strut problem - S...

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