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.

Details

Title
Comparison Virtual Landing Gear Drop Test for Commuter Aircraft Utilize MSC ADAMS And Solidworks Motion Analysis
Author
Hidayat, Dony 1 ; Istiyanto, Jos 2 ; Danardono Agus Sumarsono 2 

 Aeronautics Technology Center, National Institute of Aeronautics and Space (LAPAN), Indonesia; Department of Mechanical, Faculty of Engineering, Universitas Indonesia, Indonesia 
 Department of Mechanical, Faculty of Engineering, Universitas Indonesia, Indonesia 
Publication year
2018
Publication date
Apr 2018
Publisher
IOP Publishing
ISSN
17426588
e-ISSN
17426596
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
2572199074
Copyright
© 2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.