Structural analysis and design of airplanes (1920)
United States. Army. Air Corps · [Washington] · leaf 189
ding byabsorbing the kinetic energy of the airplane which is falling with a cer-tain vertical velocity. The energy thus taken up by each strand of cordequals the elongation of the cord times the average tension in the cordduring this elongation. For example, assume that the airplane used inthis… … Fig. 103 170 Art. 123 Design of the Shock Absorber tf v: :: T-£ ~t X X H^ _(__. _t_^u_4 + .._ - V ^_^_ --^■-^ - - j n X it 1 x . + ^ 2 t -■H- t....... .4 f. y 4-^ 1- r -j «::_:_: x -+- - l- -^ >::__:_ ___ _:_:_: x __: z f <: -4- -^ -(. --_- y- 3 2 t C 3:: : :: . x ^ • 2 j. !f:: . -__ _: -…
Airplanes
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