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Shape Optimization of Wing Structures with Aeroelastic Constraints

Schwochow, J. and Klimmek, Th. (2001) Shape Optimization of Wing Structures with Aeroelastic Constraints. CEAS Conference on Multidisciplinary Optimization, Köln/Germany, 25-26 Juni 2001.

Full text not available from this repository.

Abstract

A strategy is presented to optimize wing structures under static aeroelastic constraints with respect to parameters defining wing shape and structural layout. The aerodynamic and structural models are based on one common parameterized geometry description. While the aerodynamic model includes the description of the three dimensional surface geometry, the structural model description is based on the Finite Element Method and includes a detailed wing layout concept with arbitrarily oriented spars and ribs. The aeroelastic toolkit ZAERO employs the modal formulation for solving the trim problem of the flexible aircraft and calculates the loads for selected trim cases. The optimization framework is integrated in the design system iSIGHT which finds the optimal wing planform under given mass and aeroelastic constraints. In two design studies the wing sweep and aspect ratio are varied and the convergence performance of the framework is shown.

Item URL in elib:https://elib.dlr.de/14518/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Shape Optimization of Wing Structures with Aeroelastic Constraints
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schwochow, J.UNSPECIFIEDUNSPECIFIED
Klimmek, Th.UNSPECIFIEDUNSPECIFIED
Date:2001
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 199-208
Status:Published
Keywords:Aeroelastic Wing Design, Aeroelastic Trim Analysis, CAGD, MDO, NURBS, Structural Optimization
Event Title:CEAS Conference on Multidisciplinary Optimization, Köln/Germany, 25-26 Juni 2001
Organizer:CEAS/DGLR
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:57

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