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Landing Gear Positioning and Structural Mass Optimization for a Large Blended Wing Body Aircraft

Cumnuantip, Sunpeth (2014) Landing Gear Positioning and Structural Mass Optimization for a Large Blended Wing Body Aircraft. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-20, 139 S.

Full text not available from this repository.

Abstract

A landing gear conceptual configuration for a large Blended Wing Body (BWB) Aircraft is proposed. The investigations are based on an integrated Multidisciplinary Optimization process for the design. Multi-Body Simulation is used to determine the dynamic ground loads of the BWB. Focus is on the assessment of the effect of ground loads on the aircraft structure and on the landing gear weight. Finally, an optimized landing gear layout (number and position of landing gears) is proposed for the BWB.

Item URL in elib:https://elib.dlr.de/94582/
Document Type:Monograph (DLR-Forschungsbericht, Dissertation)
Title:Landing Gear Positioning and Structural Mass Optimization for a Large Blended Wing Body Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Cumnuantip, Sunpethsunpeth.cumnuantip (at) dlr.deUNSPECIFIED
Date:July 2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:139
ISSN:ISSN 1434-8454
Status:Published
Keywords:Aircraft Landing Gear Conceptual Design, Blended Wing Body Aircraft, Multi-Body Simulation, Multidisciplinary Optimization
Institution:Institut für Aeroelastik
Department:Lastanalyse und Entwurf
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 - Concepts and Integration
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Cumnuantip, Sunpeth
Deposited On:13 Jan 2015 14:51
Last Modified:13 Jan 2015 14:51

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