Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear
Usually during the design of landing gear, simplified Finite Element (FE) models, based on one-dimensional finite elements (stick model), are used to investigate the in-service reaction forces involving each subcomponent. After that, the design of such subcomponent is carried out through detailed Gl...
Saved in:
Main Authors: | F. Caputo, A. De Luca, A. Greco, A. Marro, A. Apicella, R. Sepe, E. Armentani |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2018-01-01
|
Series: | Advances in Materials Science and Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/8536581 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Numerical Prediction of Fatigue Life for Landing Gear Considering the Shock Absorber Travel
by: Haihong Tang, et al.
Published: (2025-01-01) -
Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model
by: Hakan Yazici, et al.
Published: (2016-01-01) -
Identification of a Non-Linear Landing Gear Model Using Nature-Inspired Optimization
by: Felipe A.C. Viana, et al.
Published: (2008-01-01) -
Approach and Landing Aircraft Wake Encounter Risk Based on Reynolds-Averaged Navier-Stokes Numerical Simulation
by: Weijun Pan, et al.
Published: (2022-01-01) -
Adaptive Landing Gear: Optimum Control Strategy and Potential for Improvement
by: Grzegorz Mikułowski, et al.
Published: (2009-01-01)