- #1
masterchiefo
- 212
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Homework Statement
The landing gear of an aircraft is composed of a main leg OA (with a weight including the wheel is
1000N to G) and two secondary links BC and 50cm long each CD. The DC link forms an angle
θ of 30 degrees with the vertical.
a) Add the rotational equilibrium equation with respect to fulcrum A of
forces acting (only) on the leg OA and determine the force
exerted by the DC link D.
Pic in attachment.
Homework Equations
The Attempt at a Solution
sin(x)=40/80 = 30 degree
Total forces X : DC *cos(30) - w*sin(30) = 0
Total forces in Y: DA+DC*sin(30)-w*cos(30)=0
Moment of force(total) = 0.80m*DC*cos(30)+0-w*sin(30) = 0
I have a problem with my Moment of force equation, I am missing something or something is wrong because my calculator gives me an error "FALSE".
Took a good 2 hours to try to figure out by my own but I did not find my error.
Thank you for helping.