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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 ...
17 maj 2022 · Aircraft Landing Gear Design. The landing gear, or undercarriage, has two primary requirements: to support the aircraft while on the ground and to absorb the large landing loads.
landing calculation when it comes to calculating the allowed approach speed from which the pilot can flare out the approach (making the downward flight path horizontal) and touch down without damage to the rear fuselage.
1 paź 2020 · The paper presents a preliminary calculation method, which is easy to apply for pre-dimensioning the landing gear. Preliminary calculation of the landing gear includes estimating the loads...
LANDING GEAR HEALTH MONITORING AS COMPLEMENTARY TEST METHOD. LANDING GEAR TESTING AS PART OF STRUCTURAL TESTING. eVTOL AIRCRAFT AS MARKET AND CERTIFICATION EXAMPLE. SUMMARY. Landing gear (L/G) is one of the key safety component of the aircraft enabling take-off, landing, and ground manoeuvres.
Preliminary calculation of the landing gear includes estimating the loads on landing and determining the position of the nose landing gear and the main landing gear of a military training aircraft.
