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Flight Loads Analysis with Inertially Coupled Equations of Motion

Reschke, Christian (2005) Flight Loads Analysis with Inertially Coupled Equations of Motion. Proc. of AIAA Atmospheric Flight Mechanics Conference, 2005-08-15 - 2005-08-18, San Francisco.

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Abstract

In this work an approach for simulation of a large passenger aircraft with high precision equations of motion and a new method of dynamic loads calculation is presented, which can be used for maneuver and gust loads analysis in the time domain. Equations of motion and equations of structural loads are derived from first principles. The consistent set of equations includes all inertial coupling terms and is tailored for direct integration of finite element models. A dynamic simulation of a large transport aircraft is used to show the influence of inertial coupling terms on simulation and loads computation.

Item URL in elib:https://elib.dlr.de/19125/
Document Type:Conference or Workshop Item (Paper)
Additional Information:LIDO-Berichtsjahr=2005, monograph_id=AIAA-2005-6026,
Title:Flight Loads Analysis with Inertially Coupled Equations of Motion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Reschke, ChristianUNSPECIFIEDUNSPECIFIED
Date:August 2005
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Equations of Motion, Force Summation Method, Inertial Coupling, Flight mechanics, Aeroelasticity, Simulation
Event Title:Proc. of AIAA Atmospheric Flight Mechanics Conference
Event Location:San Francisco
Event Type:international Conference
Event Dates:2005-08-15 - 2005-08-18
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics (until 2012)
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Feb 2006
Last Modified:31 Jul 2019 19:15

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