Results 11 to 20 of about 310,977 (203)
Bifurcation Analysis of a Coupled Nose-Landing-Gear–Fuselage System [PDF]
Journal of Aircraft, 2014 Under certain conditions during takeoff and landing, pilots may sometimes experience vibrations in the cockpit. Because the cockpit is located right above the nose landing gear, which is known to potentially be prone to self-excited vibrations at certain velocities, an explanation for those vibrations might be oscillations of the landing gear feeding ...
Terkovics, Nandor +3 more
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Bifurcation Analysis of Nose-Landing-Gear Shimmy with Lateral and Longitudinal Bending [PDF]
Journal of Aircraft, 2010 This work develops and studies a model of an aircraft nose landing gear with torsional, lateral, and longitudinal degrees of freedom. The corresponding three modes are coupled in a nonlinear fashion via the geometry of the landing gear in the presence of a nonzero rake angle, as well as via the nonlinear tire forces.
Thota, P, Krauskopf, B, Lowenberg, MH
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International Journal of Aerospace Engineering, 2019 The modern undercarriage system of a large aircraft normally requires the landing gear to be retractable. The nose landing gear, installed in the front of the fuselage, is retracted either forward or rearward.
Yong Liang +4 more
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Simulation of Nose Landing Gear Shimmy with Flexible Airframe Considered [PDF]
Xibei Gongye Daxue Xuebao, 2018 Shimmy stability of the nose landing gear of an aircraft is studied in this paper. Firstly, Shimmy model was built considering the dynamic characteristics of the airframe. Then the critical damping, critical velocity and frequency range of the shimmy are
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Dynamic Testing and Fatigue Analysis of the I-31P Nose Landing Gear [PDF]
Fatigue of Aircraft Structures, 2023 The landing gear is a critical safety component of any aircraft, playing a key role in managing the significant loads experienced during landing and ground maneuvers. In the case of the I-31P aircraft, a redesign of the I-23 landing gear system, required
Skorupka Zbigniew
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Study on stiffness and shimmy stability of strut-type nose landing gear system
Hangkong gongcheng jinzhan, 2023 System stiffness (longitudinal, lateral, and torsional stiffness) is a meaningful index for strut nose landing gear design.It arises from profound significance to explore the influence law of system stiffness on shimmy stability for the anti-shimmy ...
FENG Guang +5 more
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Preliminary calculation of the landing gear of a military training aircraft [PDF]
INCAS Bulletin, 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 on landing and determining the position of the nose landing gear ...
Ilie NICOLIN, Bogdan Adrian NICOLIN
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Design and Analysis Aircraft Nose and Nose Landing Gear [PDF]
Journal of Aeronautics & Aerospace Engineering, 2015 Tri-cycle arrangement landing gear is extensively used as it is simple; convenient both structurally as well as aerodynamically. Though it is advantageous over other configuration is has its own draw backs. Factors like its weight drag, sudden application of load, acoustics, fatigue etc tend to slow down its performance and life.
Rajesh A, Abhay BT
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Bifurcation Analysis of a Nose Landing Gear System [PDF]
15th Dynamics Specialists Conference, 2016 A methodology is proposed to enable the bifurcation analysis of a multi-body nose landing gear (NLG) model by coupling AUTO, a continuation software, to LMS Virtual.Lab Motion, a multi-body software. The approach uses a Singular Value Decomposition (or High Order Singular Value Decomposition) based technique to enable the computation of the stability ...
Tartaruga, Irene +4 more
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Shimmy analysis of light weight aircraft nose wheel landing gear [PDF]
, 2022 This paper presents mathematical modeling and analysis of shimmy oscillations for a light weight airplane single wheel nose landing gear. Shimmy is a self-excited oscillation which occurs usually on the nose wheel landing gear assembly during ground ...
Giridharan, V., Sivakumar, S.
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