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Application of a Flexible Wing Modeling and Physical Mass Estimation System for Early Aircraft Design Stages

Dorbath, Felix and Nagel, Björn (2014) Application of a Flexible Wing Modeling and Physical Mass Estimation System for Early Aircraft Design Stages. 73rd Annual Conference of Society of Allied Weight Engineers, 17. - 21. Mai 2014, USA, Los Angeles.

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Item URL in elib:https://elib.dlr.de/134600/
Document Type:Conference or Workshop Item (Speech)
Title:Application of a Flexible Wing Modeling and Physical Mass Estimation System for Early Aircraft Design Stages
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Dorbath, Felixfelix.dorbath (at) dlr.deUNSPECIFIED
Nagel, BjörnBjoern.Nagel (at) dlr.dehttps://orcid.org/0000-0001-8076-9853
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Flexible, Wing, Modeling, Physical, Mass Estimation, Early Aircraft
Event Title:73rd Annual Conference of Society of Allied Weight Engineers
Event Location:USA, Los Angeles
Event Type:international Conference
Event Dates:17. - 21. Mai 2014
Organizer:SAWE
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: Hamburg
Institutes and Institutions:Air Transport Operations > Integrated Aircraft Design
Deposited By: Hagemann, Maice
Deposited On:09 Apr 2020 08:57
Last Modified:09 Apr 2020 08:57

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