Results 41 to 50 of about 416,562 (354)

Analysis of aerodynamic and aeroacoustics of full scale landing gear

open access: yesXibei Gongye Daxue Xuebao, 2022
The aerodynamic noise of a landing gear is an important source of airframe noise. The analysis of its noise characteristics plays an important role in the design of a low-noise landing gear.
TIAN Siyuan   +5 more
doaj   +1 more source

Landing Performance Study for Four Wheels Twin Tandem Landing Gear Based on Drop Test

open access: yesAerospace, 2022
The drop tests of a twin tandem landing gear with different filling parameters are carried out in two different landing attitudes (level and tail-down). The overload coefficient and power absorption efficiency are obtained.
Wei-Dong Fang, Ling Zhu, Youshan Wang
semanticscholar   +1 more source

Selection Methodology of Composite Material for Retractable Main Landing Gear Strut of a Lightweight Aircraft

open access: yesApplied Sciences, 2022
The design and development of high-strength and low-weight composite landing gear struts is still a challenge in today’s world. In this study, a selection methodology for fiber-reinforced composite material for retractable main landing gear struts for ...
Muhammad Ayaz Ahmad   +5 more
doaj   +1 more source

Simulation of Runway Irregularities in a Novel Test Rig for Fully Electrical Landing Gear Systems

open access: yesAerospace, 2022
The E-LISA research project, under way within the Clean Sky 2 framework, has the objective of developing an innovative iron bird dedicated to executing tests on the landing gear of a small aircraft transport equipped with an electro-mechanical landing ...
Andrea De Martin, G. Jacazio, M. Sorli
semanticscholar   +1 more source

Structure design and breakaway failure analysis of fuse-pin for civil main landing gear

open access: yesHangkong gongcheng jinzhan
The landing gear should be able to achieve safe and rapid separation from the aircraft body under overload conditions. To clarify the effect of breakaway groove on the breakaway load of emergency fuse-pin for civil main landing gear, a series of FEM ...
FU Liang   +5 more
doaj   +1 more source

Preliminary Estimation Methods for the Definition of the Landing Gear [PDF]

open access: yesINCAS Bulletin, 2018
The landing gear of an aircraft is an important part of the aircraft structure. The landing and the taking off are most critical parts of a flight mission.
Daniela BARAN   +2 more
doaj   +1 more source

Research on the Influence of Temperature on the Cushioning Performance of Oil-air Landing Gear

open access: yesHangkong gongcheng jinzhan, 2022
The oil characteristics and inflation pressure inside the oil-air shock absorber will change with the ambient temperature,which will affect the cushioning performance of landing gear.In order to explore the effect of temperature on the cushioning ...
HU Rui, MU Rangke, SONG Dejun, CHEN Yi
doaj   +1 more source

Shape memory alloy based smart landing gear for an airship [PDF]

open access: yes, 2007
The design and development of a shape memory alloy based smart landing gear for aerospace vehicles is based on a13; novel design approach. The smart landing gear comprises a landing beam, an arch, and a superelastic nickeltitanium shape memory alloy ...
Dayananda, GN   +2 more
core   +1 more source

Analisis Frekuensi Natural Rangka Main Landing Gear Pesawat UAV Menggunakan Ansys Workbench

open access: yesJurnal Mesin Nusantara, 2022
The main landing gear is one of the important components in UAV aircraft. This paper aims to analyze the natural frequency of the main landing gear and determine its normal mode shape.
Lasinta Ari Nendra Wibawa
semanticscholar   +1 more source

Study on Landing Gear’s Load for Airship Based on the Double-springs’ Vibration Model

open access: yesHangkong gongcheng jinzhan, 2020
The FAA-P-8110-2 Airship Design Criteria defines the airworthiness standard requirement. In order to make the design of landing gear to fulfill the requirements perfectly, a methodology of load calculation for landing gear is presented in this paper ...
HU Xiaojin, XIAO Peng, HE Wei
doaj   +1 more source

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