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, 2014-05-17 - 2014-05-21, USA, Los Angeles.

Full text not available from this repository.

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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Dorbath, Felix	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Nagel, Björn	UNSPECIFIED	https://orcid.org/0000-0001-8076-9853	UNSPECIFIED

Date:

2014

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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 Start Date:

17 May 2014

Event End Date:

21 May 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 (old)

Location:

Hamburg

Institutes and Institutions:

Air Transport Operations > Integrated Aircraft Design

Deposited By:

Hagemann, Maice

Deposited On:

09 Apr 2020 08:57

Last Modified:

24 Apr 2024 20:37

Repository Staff Only: item control page