Analysis of Landing-Gear Behavior
Citations
8 citations
Cites background from "Analysis of Landing-Gear Behavior"
...The part of the fuselage on each gear can be considered as a rigid mass since the main gears of the aircraft are mostly located near the nodal points of the wing bending modes and consequently landing gear performance is not affected by the elastic deformation of the aircraft structure [10]....
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8 citations
8 citations
8 citations
Cites methods from "Analysis of Landing-Gear Behavior"
...The research of aircraft landing gear operation with an oil-pneumatic (oilgas) damper is also described in work [28]....
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References
5 citations
"Analysis of Landing-Gear Behavior" refers background or methods in this paper
...In addition to the total fo,'ce on the upper mass, figure 4 Ca) presents calcLdatcd time histories of the hydraulic and pneumatic components of the shock-strut force, as determined from equations (2) and (3), respectively....
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...Equation (2) can be nlade applicable to both tile compression and elongation strokes by introducing tlle factor 7; to indic....
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