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the total aerodynamic force F acting on the airplane has a magnitude of 6250 N. Resolve this force into vertical and horizontal components.(called the lift and the drag, respectively).
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do u hv lr fig?
clear figure
|dw:1371400866475:dw|
can u understand the figure? i don't know how to draw an airplane. :))))))
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no its ohk ill c the qstn is confusing me gv me sum tym is der any other dtail givn
there's no other detail given..
ohhh
arent d components given that is I i j k I compo
do you know the ans?
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|dw:1371402174897:dw|
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