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24 gru 2022 · 1- Drag coefficient for a retractable landing gear. I tried the following equations: CD,gear = WingLoading * FlapDeflection * (( AircraftMass(TO,LD))^-0.215) CD0,gear = SUM i=1 > n [CD,gear(AreaLG / WingArea)] The results were ASTRONOMICAL. 2- Weight of main and nose landing gears.
22 sie 2019 · Hi there, I am working on the project regarding the landing gear structural analysis. I have gone through the FAR part 25 for the ground loads. The load cases seem quite reasonable, the only problem is that I am not sure how these should be calculated for a given aircraft. The part I find confusing is that I am not sure which loads can be ...
Landing gear design is ruled by a set or requirements. Some of them are common for all transport aircraft as the they are defined in the airworthiness requirements of FAA and EASA.
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17 maj 2022 · The landing gear, or undercarriage, has two primary requirements: (1) to support the aircraft while on the ground and (2) to absorb the large loads associated with landing, and transfer these from the wheels to the aircraft’s primary structure.
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17 gru 2020 · We have 94 Aircraft Landing Gear For Sale. Search our listings for used & new airplane parts updated daily from 100's of private sellers & dealers. 1 - 24.
