Wheel dynamometer system for aircraft landing gear testing-Reference-Cited by-同舟云学术

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Wheel dynamometer system for aircraft landing gear testing

Published:2019-12 Issue: Volume:148 Page:106918
ISSN:0263-2241
Container-title:Measurement
language:en
Short-container-title:Measurement

Author:

Pytka Jarosław,Józwik Jerzy,Budzyński Piotr,Łyszczyk Tomasz,Tofil Arkadiusz,Gnapowski Ernest,Laskowski Jan

Funder

Polish Ministry of Science and Higher Education

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference20 articles.

1. Overview of landing gear dynamics;Pritchard;J. Aircraft,2001

2. Aircraft landing impact parametric study with emphasis on nose gear landing conditions;Chester;J. Aircraft,2002

3. Dynamic analysis of aircraft landing impact using landing-region-based model;Wei;J. Aircraft,2005

4. Improved model of landing-gear drop dynamics;Wei;J. Aircraft,2014

5. Method for testing and evaluating grassy runway surface;Pytka;J. Aircraft,2017

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4. Design and Calibration of a Novel Multi-Axis Sensor for Measuring the Wheel-Terrain Interaction Forces of Robotic Vehicles;2024

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