2011•Unpublished venueRequires access

Simulation of Landing Gear Drop Considering Flexible Airframe

Avic Aircraft

Open publisher page 0 citations

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 two results,it shows that the flexible peak load is lower than the rigid one,and the landing gear energy absorb chart becomes more gently.This method can thus provide more accurate design reference for landing gear design.

About this research paper

What this paper is about

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 two results,it shows that the flexible peak load is lower than the rigid one,and the landing gear energy absorb chart becomes more gently.This method can thus provide more accurate design reference for landing gear design.

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available 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 two results,it shows that the flexible peak load is lower than the rigid one,and the landing gear energy absorb chart becomes more gently.This method can thus provide more accurate design reference for landing gear design.

Key concepts: Airframe, Landing gear, Drop test, Drop (telecommunication), Engineering, Modal, Chart, Simulation

Related papers

Back to paper searchBrowse research topicsOriginal source
Simulation of Landing Gear Drop Considering Flexible Airframe — Research Paper | ScholarLens