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Multi-fidelity Mass Estimation of a Strut-Braced Wing Configuration

Böhnke, Daniel and Dorbath, Felix and Nagel, Björn (2014) Multi-fidelity Mass Estimation of a Strut-Braced Wing Configuration. EASN Flight Physics Workshop, 27.-29. September 2014, Deutschland, Aacen.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/134545/
Document Type:Conference or Workshop Item (Speech)
Title:Multi-fidelity Mass Estimation of a Strut-Braced Wing Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Böhnke, DanielDaniel.Boehnke (at) dlr.deUNSPECIFIED
Dorbath, Felixfelix.dorbath (at) dlr.deUNSPECIFIED
Nagel, BjörnBjoern.Nagel (at) dlr.dehttps://orcid.org/0000-0001-8076-9853
Date:27 September 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Mulit-Fidelity, Strut-Braced Wing Configuration
Event Title:EASN Flight Physics Workshop
Event Location:Deutschland, Aacen
Event Type:Workshop
Event Dates:27.-29. September 2014
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 09:04
Last Modified:09 Apr 2020 09:04

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