elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Assessment of Dynamic Landing Loads by a Hybrid Multibody / Full Finite Element Simulation Approach

Cumnuantip, Sunpeth and Krüger, Wolf R. (2018) Assessment of Dynamic Landing Loads by a Hybrid Multibody / Full Finite Element Simulation Approach. DLRK 2018 - Deutscher Luft-und Raumfahrt Kongress, 04.-06. Sep. 2018, Friedrichshafen, Deutschland. DOI: 10.25967/480116

[img] PDF
3MB

Official URL: http://publikationen.dglr.de/?tx_dglrpublications_pi1[document_id]=480116

Abstract

This paper describes a new process for the detailed assessment of the impact of aircraft ground manoeuvres on local structural loads. The process is comprised of two core elements, a multibody simulation analysis and a subsequent direct transient response finite element analysis. The multibody simulation is used for the simulation of aircraft landing loads. These loads are then applied to an aircraft finite element model, via a direct transient response, for a more detailed analysis of the aircraft dynamic behavior at the desired points of interest. The process has been developed using landing simulations of two reference aircraft with their corresponding finite element models. The objective of the current activities is to study the effect of major simulation and modelling parameters on the detailed aircraft dynamic response. In the paper, the process and the results of the parameter studies will be presented.

Item URL in elib:https://elib.dlr.de/122778/
Document Type:Conference or Workshop Item (Speech)
Title:Assessment of Dynamic Landing Loads by a Hybrid Multibody / Full Finite Element Simulation Approach
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Cumnuantip, SunpethInsitute of Aeroelasticity, German Aerospace Center (DLR)UNSPECIFIED
Krüger, Wolf R.Insitute of Aeroelasticity, German Aerospace Center (DLR)UNSPECIFIED
Date:October 2018
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.25967/480116
Status:Published
Keywords:dynamic landing loads, multibody simulation, transient finite element analysis
Event Title:DLRK 2018 - Deutscher Luft-und Raumfahrt Kongress
Event Location:Friedrichshafen, Deutschland
Event Type:national Conference
Event Dates:04.-06. Sep. 2018
Organizer:DGLR - Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Cumnuantip, Sunpeth
Deposited On:21 Nov 2018 11:09
Last Modified:31 Jul 2019 20:20

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.