Comparison Virtual Landing Gear Drop Test for Commuter Aircraft Utilize MSC ADAMS and Solidworks Motion Analysis

Research output: Contribution to journalConference articlepeer-review

Abstract

Loads at main landing gear while touchdown impact is function of aircraft weight and ground reaction load factor. In regulation states ground reaction load factor at Vsink = 3.05 m/s is below 3. Contact/impact force from simulation using MSC ADAMS is 94680 N, while using Solidworks Motion Analysis is 97691 N. The difference between MSC ADAMS and Solidworks Motion Analysis is 3.08%. The ground reaction load factor in MSC ADAMS is 2.78 while in Solidworks Motion Analysis is 2.87.

Original languageEnglish
Article number012007
JournalJournal of Physics: Conference Series
Volume1005
Issue number1
DOIs
Publication statusPublished - 4 May 2018
Event5th International Seminar on Aerospace Science and Technology, ISAST 2017 - Medan, North Sumatra, Indonesia
Duration: 27 Sep 201729 Sep 2017

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