Evaluation and Uncertainty Quantification of Bifurcation Diagram: Landing Gear, a Case Study

doi 10.7712/120215.4307.512
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens (NTUA) Greece

Related search

Bifurcation Analysis of a Coupled Nose-Landing-Gear–Fuselage System

Journal of Aircraft
Aerospace Engineering
2014English

Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System

2012English

Aeroacoustics of a Landing Gear Door

2013English

Linear Buckling Analysis of Landing Gear

International Journal of Engineering and Advanced Technology
EngineeringComputer Science ApplicationsEnvironmental Engineering
2019English

Vibration Control of MR Damper Landing Gear

International Journal of Advanced Research in Artificial Intelligence
2013English

A Validation Study of Higher Order CFD Analysis for Unsteady Flow Around Landing Gear

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
2011English

Fluid Similarity Criterions in Aircraft Landing Gear

MATEC Web of Conferences
Materials ScienceEngineeringChemistry
2018English

Complex Landing Gear Noise Prediction Using a Simple Toolkit

2005English

Gear Contact Fatigue Failure Effects Evaluation Under Process Uncertainty Influence.

English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy