Simulation of Landing Gear Drop Considering Flexible Airframe

Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University

Home > Archive>Volume 2, Issue 2, 2011 >

PDF HTML XML Export Cite reminder

Simulation of Landing Gear Drop Considering Flexible Airframe
DOI:
                        
CSTR:
                        
Author:
                        
Affiliation:Liu Chongchong,Mu Rangke,Ma Xiaoli,Liu Xiaochuan(AVIC Aircraft Strength Research Institute,Xi'an 710065,China)
Clc Number:V214 TP391.9
Fund Project:

Article

Figures

Metrics

Reference

Cited by

Materials

Comments

Abstract:

The finite element model of flexible airframe is created firstly,its mode coincide with leuven modal test system(GVT) test.Then the buffer force is analyzed and program is compiled to calculate the relevant curve.On the LMS simulation platform a single landing gear drop is simulated by using this curve.Based on the single landing gear drop simulation,which coincides with the drop test,the whole aircraft drop test simulation is done including rigid airframe and flexible airframe.Through the comparison of the...

Reference

Cited by

Get Citation

Liu Chongchong, Mu Rangke, Ma Xiaoli, Liu Xiaochuan. Simulation of Landing Gear Drop Considering Flexible Airframe[J]. Advances in Aeronautical Science and Engineering,2011,2(2):

Copy

Article Metrics

Abstract:
PDF:
HTML:
Cited by:

History

Received:
Revised:
Adopted:
Online: January 13,2012
Published:

Get Citation

Share

Article Metrics

History

Article QR Code