Calculate the force in each member of the wing using both joint method as well a

Question

Calculate the force in each member of the wing using both joint method as well as the section method. State all the Assumptions. The picture is here :-http://www.google.ca/imgres?imgurl=http://www.steenaero.com/Images/Aircraft/skybolt_cutaway_white_1091x816.jpg&imgrefurl;=http://www.steenaero.com/Skybolt/&h;=816&w;=1091&sz;=759&tbnid;=5IQjq50wDVtWRM:&tbnh;=90&tbnw;=120&prev;=/search?q=skybolt&tbm;=isch&tbo;=u&zoom;=1&q;=skybolt&usg;=__lgzLJSgIY7R6nPfxq-Ysqy9rvds=&docid;=3uhZTGI8DL_oJM&hl;=en&sa;=X&ei;=tlytUJXxEYXriwLHxYGIBg&sqi;=2&ved;=0CEwQ9QEwBQ&dur;=288

Explanation / Answer

how do i calculate there is no other information given execpt figure.

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